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This paper addresses the critical need for accurate post-fire assessment of reinforced concrete warehouses, where fire-induced damage can compromise structural safety and repair strategies. Traditional visual inspection and conservative design assumptions often fail to capture the true extent of degradation, especially under realistic fire scenarios. To overcome these limitations, a combined computational fluid dynamics and finite-element framework that simulates the warehouse fire environment, estimates thermal exposure, and evaluates its impact on the structural response and residual capacity of damaged reinforced concrete elements is presented. Experimental diagnostics – including laser scanning, non-destructive testing, and material sampling – were conducted to calibrate the models and quantify damage. The findings highlight that the proposed methodology enables a more reliable identification of severely compromised components, supports targeted and cost-effective retrofitting interventions, and offers practical guidance for improving resilience in similar structures. This work advances performance-based fire engineering by demonstrating a validated and holistic assessment strategy that can inform reconstruction decisions and enhance fire safety practices in industrial buildings.

Fire remains one of the most critical hazards to structural safety and integrity, with a non-negligible probability of occurrence in various real-world scenarios. It is categorised as an extreme loading event, on par with blasts and impacts, as specified in several international structural design codes and standards, due to the potential severity of its effects (Ma et al., 2025). In many incidents, fires are either triggered by or lead to explosions, which subject structures to compounded thermal and mechanical loads that push materials beyond their conventional performance limits (Chen et al., 2024; Pinna et al., 2025; Pinna and Stochino, 2025; Stochino, 2016).

Among the most widely used structural materials, reinforced concrete (RC) is particularly sensitive to high-temperature exposure. Its mechanical properties, such as compressive strength, stiffness, and bond strength, deteriorate significantly with temperature rise (Çelik and Urtekin, 2025; Jiao et al., 2014; Saeed and Al-Ahmed, 2025). To capture this behaviour, a variety of thermo-mechanical models have been developed and validated against experimental data (Li et al., 2004). However, accurate structural assessment after a fire event demands more than just knowledge of material degradation, as well as requires reconstructing the temperature–time history and understanding the evolution of stress and strain fields during and after exposure (La Scala et al., 2024a; Osman et al., 2017).

Therefore, the importance of performance-based fire engineering is gaining momentum, in which the prime objective is to evaluate structural performance under realistic fire conditions rather than just following prescriptive regulations. Using well-documented case studies can improve this method by giving accurate information about temperature changes and how structures react (Gernay, 2024).

In this context, modern computational tools play a pivotal role. Computational mechanics, particularly finite-element (FE) analysis and computational fluid dynamics (CFD), offers robust and flexible methods to simulate the highly non-linear and time-dependent behaviour of materials and structures under fire conditions (La Scala et al., 2023; 2024b).

CFD (McGrattan and Miles, 2016), which centres on the numerical solution of the Navier–Stokes equations (Chorin, 1968), is a powerful tool for simulating the complex behaviour of fluids and gases under a wide range of physical conditions. In the context of fire engineering, CFD enables highly detailed modelling of key phenomena such as heat transfer through convection and radiation, flame propagation, smoke movement, and fluid–structure interactions (Wen, 2024). These processes are inherently non-linear and often occur simultaneously in highly dynamic and geometrically complex environments, such as multi-room buildings, tunnels, or industrial facilities. Analytical solutions to the Navier–Stokes equations are only feasible for very simple and idealised problems due to the non-linear nature of the equations and the wide range of boundary conditions encountered in real-world scenarios.

Fires create turbulent airflow and have material properties that change with temperature. The changing conditions in fire scenarios make analytical solutions difficult, so CFD-based numerical methods are essential for accurately modelling the interactions between fire and structural responses (Maragkos and Beji, 2021).

Recent advancements in post-fire safety assessment of RC structures demonstrate the effective integration of experimental and computational approaches.

Khan et al. (2021) review the evolution and current state of fire models for structural fire assessment, focusing on gas temperature predictions and their role as ‘loads’ on structures. It also explores recent advances in CFD-FEM coupling for more realistic fire–structure interaction simulations. A new methodology for the mechanical and thermal design of composite slabs under fire is proposed in Bolina and Rodrigues (2022) following a thorough numerical modelling of this problem. These studies highlight the importance of combining experimental validation with advanced computational models to accurately assess and enhance the post-fire safety of RC structures.

In addition, many interesting case study of post-fire assessment can be found in recent literature: Raposo et al. (2025) investigate the causes of a house fire in Arganil, Portugal, identifying construction flaws, materials, and heat sources to prevent similar incidents in the future. A comprehensive review on fire damage assessment of RC structures is presented in Qin et al. (2022) with specific attention to damage assessment measures for RC structures.

Despite the growing adoption of computational techniques for structural fire engineering, a significant research gap persists in the integration of experimental diagnostics with advanced numerical modelling (Yan et al., 2024) for real-world post-fire assessments. Most existing studies either focus on idealised laboratory scenarios or adopt oversimplified thermal boundary conditions in structural models, failing to reflect the complexity and heterogeneity of actual fire events in large-scale RC structures. Furthermore, limited case studies combine in situ material testing, microstructural analyses, and CFD-informed FE simulations in a unified framework. This paper addresses this gap by presenting a comprehensive investigation of a fire-damaged RC warehouse, coupling non-destructive and destructive testing, mineralogical and thermal analysis, and high-fidelity CFD and FE modelling. The aim is to develop a practical methodology for reliable post-fire safety assessments and to inform effective retrofitting strategies based on realistic thermal and mechanical behaviour.

Indeed, in this study, a coupled approach combining CFD and FE analysis is applied to a real-world case involving a RC structure that sustained significant damage due to fire. The CFD model is used to simulate the thermal environment during the fire, including temperature distribution and heat fluxes on the surfaces of structural elements. This thermal data is then used as input for the FE analysis, which models the structural response of the RC components, taking into account temperature-dependent degradation in material properties such as strength and stiffness. By integrating these two advanced computational techniques, this paper proposes a coupled simulation framework to assess thermal exposure and structural degradation in fire-damaged buildings, enhancing our understanding of fire-induced failures and aiding in performance-based fire design. Ultimately, the insights gained contribute to more informed decision making in post-fire structural assessments and promote the design of safer, more resilient built environments.

This paper is structured as follows: after this brief introduction, Section 2 provides comprehensive data on the building’s construction. Section 3 offers a review of the fire impact. Section 4 discusses the findings derived from CFD and FE modelling. Finally, Section 5 concludes the paper with key remarks and insights.

The structure under investigation is a precast pre-stressed RC warehouse built in 2010 in the outskirts of Cagliari (Italy). It consists of a single building with a footprint of approximately 60 m × 40 m (of total surface area of 2400 m2) and a height slightly over 11 m. The ground floor has a clear ceiling height of about 6 m and is divided into three compartments of approximately 800 m2 each. Whereas the first floor is an open space with a total surface area of 2400 m2, with a clear ceiling height of approximately 3.50 m. Notably, the load-bearing structure comprises (1) columns made of vibrated RC with a rectangular cross-section. Three types can be identified based on their dimensions: (a) 0.68 × 0.50 m, (b) 0.90 × 0.50 m, and (c) 0.50 × 0.50 m; (2) Rectangular pre-stressed concrete beams of type TR, with approx. 0.80 m × 0.90 m (see Figure 1(a)); (3) Ribbed ‘omega’ beams approximately 2.55 m wide (see Figure 1(b)).

On the other hand, the roofing is made using TH 120 type pre-stressed RC beams with Aliant 2 type elements, see Figure 2(a).

The floor system consists of precast panels joined to supporting beams through a cast-in-place concrete slab. It is designed to support a total load of 850 kg/m2, comprising 400 kg/m2 of live load and 200 kg/m2 of dead load, whereas 250 kg/m2 is the load of the 10-cm-thick RC slab. The vertical enclosure comprises panels anchored at the base to the foundations or portal frames, and at the top to the perimeter beams. This configuration enables the transfer of horizontal forces while allowing for longitudinal movement, thereby preventing the transmission of vertical loads.

According to the original design, characteristic compressive concrete strength is 46 N/mm2, while reinforcement bars are characterised by a yielding strength of 430 N/mm2 and a tensile strength of 540 N/mm2 in the case of a diameter smaller than 12 mm; otherwise yielding strength is 430 N/mm2 and tensile strength 480 N/mm2. Moreover, pre-stressing tendons of the beams are characterised by a diameter of 3/8” (9.5 mm) and 1/2” (12.7 mm); their tensile strength is 1860 N/mm2. More information about the structure characteristics can be found in Stochino et al. (2017a).

On the evening of 16 November 2013, a fire broke out on the ground floor, causing significant structural damage, as shown in Figure 3. Notably, the fire was contained to the central area of the ground floor and did not extend to other parts of the building (see Figure 4).

The presence of fire-resistant partition walls prevented the fire that broke out in one compartment from spreading to the others. The focus was therefore placed solely on the compartment affected by the flames. The fire completely destroyed both the interior spaces and the systems within the affected compartment, while the exterior facade shows no visible or apparent damage. The large amount of combustible material in the warehouse led to the fire’s rapid development and swift spread. The damage was first analysed in the study, and the related data were recorded to assess the degree of structural degradation. Based on the analyses carried out, it was concluded that although the damage caused by the fire was severe, with appropriate restoration work, it is possible to return the structure to its previous condition.

After the fire, a substantial amount of debris was observed across almost the entire floor area. This debris consisted primarily of fragmented concrete, remnants of steel shelving units, charred wooden pallet pieces, and other fire-generated residues (Figure 5). The distribution and quantity of the debris suggest an intense fire that was localised in certain areas, causing widespread disintegration of both non-structural and structural elements, see Figure 5.

A detailed inspection of the structural frame revealed that the lateral columns identified as 4, 6, 7, and 9 (Figure 6) sustained the most extensive damage. Visual examination reveals that these columns were subjected to severe thermal exposure on one side, resulting in progressive material degradation inward toward the core. This pattern of damage suggests asymmetric heating, resulting in hollowing or loss of integrity on the fire-exposed faces (Figure 6).

In contrast, the perimeter columns 1, 2, 3, 10, 11, and 12 were located far from the central fire zone, therefore experienced considerably lower thermal exposure. Notably, their physical condition remains relatively intact, with no immediate signs of critical structural compromise.

The central columns, particularly columns 5 and 8, display surface characteristics indicative of high-temperature exposure. Their exteriors show significant roughness and a distinctive greyish-white coloration, a typical sign of surface dehydration and chemical changes in concrete under intense heat (Figure 6).

Regarding the horizontal structural elements, only the lower portions of the beams were directly exposed to the fire. The upper parts remained shielded by the concrete slab, which provided some level of thermal protection. However, in several beams, specifically T3, T4, T5, T6, L4, L5, L8, and L9 severe damage has been identified (Figure 6). These include substantial spalling of the concrete cover and partial debonding or exposure of the pre-stressing tendons, both of which can significantly compromise the load-bearing capacity and long-term durability of the beams.

These findings underscore the necessity for a comprehensive structural integrity assessment, potentially necessitating extensive repair or replacement of the most heavily affected components.

To determine the extent of mechanical degradation after a fire event, it is crucial to determine the maximum temperature reached during the fire (Meloni et al., 2019). The authors have conducted a detailed geometric survey using laser scanning technology to identify permanent deformations caused by the fire. Subsequently, measurements of ultrasound wave velocity and rebound index were carried out on various structural elements. A load test was also performed on one of the most representative sections of the damaged structure. A number of cylindrical core samples were extracted from columns and slabs across different areas of the building, and a destructive compressive strength tests performed on these samples revealing that the average strength of fire-damaged precast concrete (from beams and columns) found to be about 30.5 N/mm2, while the cast-in-place concrete (from slabs) exhibited an average strength of approximately 20.0 N/mm2.

Further analyses including X-ray diffraction, differential thermal analysis (DTA), optical and scanning electron microscopy (see Table 1 (Stochino et al., 2017b)), and colorimetric tests (see Table 2) have been done, and these tests provided valuable insights into the temperatures experienced by the fire-exposed concrete. The conclusions were mainly drawn from the changes observed in the mineralogical composition and microstructure of the concrete materials. A comprehensive summary of the main findings is presented in Tables 2 and 3. Notably, Table 3 data have been used as a benchmark for the model development that will be presented in the next sections.

The fire scenario was modelled using the Fire Dynamics Simulator (FDS), a CFD tool designed to numerically solve the Navier–Stokes equations under conditions of low-speed, thermally driven flows such as those generated by smoke and heat during a fire. FDS approximates the partial differential equations governing the conservation of mass, energy, and momentum using second-order finite difference methods, solving them numerically across the mesh for each time step.

This study employs the Large Eddy Simulation (LES) approach as its solution strategy. LES focuses on resolving the larger turbulent structures influenced by the specific flow geometry, while modelling the smaller, more universal turbulence scales, which are considered independent of the particular features of the flow. The LES technique does not account for small-scale phenomena and instead relies on a simplified algorithm, based on a semi-empirical method developed by Smagorinsky (McGrattan, 2006). This approach directly incorporates the large-scale turbulence into the integration process, while the smaller turbulence structures are modelled.

The pyrolysis model in FDS utilises a one-dimensional heat transfer equation to describe conduction through solid materials. This equation is solved using finite difference techniques.

For the combustion process, this study employs the combustion mixture-fraction method.

The central compartment, illustrated in Figure 7, is treated as a single computational domain with a parallelepiped geometry. Its overall dimensions are 20.50 m (x-direction), 40.20 m (y-direction), and 6.80 m (z-direction), as shown in (Figures 4 and 6). The long sides are enclosed by REI 120-rated brick walls, while the short sides consist of prefabricated concrete panels with openings, also visible.

In the numerical model, the compartment boundaries were assumed to be adiabatic; however, special attention was devoted to the modelling of the openings, as discussed in a later section. The computational mesh comprises 4800 predominantly cubic cells (dimensions: 1.02 × 1.00 × 1.13 m). A time step of 1 millisecond (10−3 s) was selected based on a convergence study conducted across various time steps, ensuring numerical stability and accuracy with the chosen mesh.

The initial (pre-incident) conditions include an ambient temperature of 20°C, an oxygen concentration of 20.70% by volume, and standard atmospheric pressure (1 atm or 101 325 Pa). The compartment is neither served by a mechanical ventilation system, nor is it equipped with fire detection or automatic fire suppression systems.

The materials present in the domain, along with their key thermophysical properties, are summarised in Table 4.

Although the precise origin and cause of the fire remain uncertain, it is suspected that a short-circuit in the lift truck’s electrical system – located beneath beam T4 (refer to Figures 2(b) and 5(a)) – may have triggered the ignition. The heat release rate per unit area (HRRPUA) for this item was taken from Särdqvist (1993) and is shown in Figure 8.

As the fire spread to additional combustible materials in the compartment, their contributions to the overall heat release were modelled using the parameters provided in Table 4.

The fire brigade arrived on scene and managed to suppress the fire. During their intervention, they forcibly opened two doors at the lower part of the building (see Figure 2), which was modelled as occurring at t = 1200 s (20 min). As interior conditions deteriorated, making direct access unsafe, one rolling shutter was subsequently opened to allow for external hose streams. This action was simulated at t = 5400 s (90 min). However, access to the shutter was hindered by wood pallets stacked up to the ceiling and placed directly in front of the opening. Consequently, it was decided to open a series of windows located on the opposite side of the hall at a height of 4.45 m on the upper side of the plant in Figure 2 at t = 6000 s (100 min).

To monitor the thermal evolution within the compartment, 78 thermocouples were modelled. Their spatial arrangement formed an approximate 5 × 5 m mesh, with sensors positioned at various heights on the sides of beams and columns. The average temperatures recorded are depicted in Figure 9.

A notable increase in temperature is observed following the window openings at 100 min, likely due to the influx of oxygen enhancing combustion.

Development of fire within the CFD simulation is visualised in Figure 10, where flame propagation is clearly illustrated.

Table 5 presents a comparison between the maximum temperatures predicted by the numerical model and those derived from microstructural and colorimetric analyses (considered benchmarks, see Tables 2 and 4). The simulation results demonstrate good agreement with experimental data, exhibiting an average error of 15%. Given the complexity of the scenario and the number of unknown parameters, this level of accuracy is considered satisfactory.

The temperature data recorded by the thermocouples were used as input for a thermomechanical analysis conducted using SAFIR (Franssen, 2005). This approach allowed for the investigation of both the temperature distribution within the cross-section of the structural elements and their mechanical response under fire conditions. In this study, the non-linear constitutive behaviour of concrete and steel has been modelled in accordance with the provisions of EN 1992-1-2 (EN 1992-1-2, 2004).

For example, for Column 5 which was exposed to fire on all sides the maximum temperature distribution obtained from the FE thermal simulation was compared with estimates derived from the post-fire in-situ investigation (see Tables 2 and 4). The field tests made it possible to estimate the maximum temperatures reached at various depths from the column’s external surface.

Figure 11 illustrates FE temperature distribution across the cross-section of Column 5 at a height of 4.45 m, compared with the estimated maximum in situ temperature. It shows that the surface temperature of Column 5 reached approximately 600°C, while at a depth of 4 cm from the surface, the maximum temperature was around 300°C. The variations in temperature across different sides of the column can be attributed to the temperature–time history produced by the CFD fire simulation. Since the fire scenario was not symmetrical, the resulting temperature distribution is inherently non-uniform.

Figure 12 illustrates the maximum temperature distribution and the deflection–time history of beam T5 (see Figure 6), which was modelled using 32 beam elements. The varying temperature fields derived from the CFD analysis lead to different thermo-mechanical responses in each section of the beam. The beam is directly exposed to fire on its underside and lateral faces, while the ceiling slab shields the top surface. As shown in Figure 12, the highest temperature, 483°C, occurs at the bottom of the beam.

Specific attention is necessary for the lateral column 6. This rectangular column (90 × 60 cm) is characterised by the presence of an internal rainwater downpipe that channels roof runoff to the sewer system. The water contained within the downpipe likely underwent significant thermal expansion due to the fire, contributing to the spalling of a large portion of the concrete within the fire-exposed region of the column, see Figure 13.

A non-linear thermomechanical coupled analysis has been developed in ANSYS to describe this phenomenon. The input temperatures were obtained by the CFD analysis presented in Section 4.3. Figure 14 shows the colour scale distribution of temperatures at the various loading steps. At 455 s, heat is concentrated near the lower boundary with minimal spread. By 6415 s, heat started propagating upward. At 10 000 s, the structure shows widespread heating, with the highest temperatures near the heat source.

From Figure 15, it is possible to observe how the column deforms in response to the applied thermal and structural loads. Initially, the deformation of the column is due solely to the structural load. As the temperature increases, thermal stress becomes more significant, leading to a noticeable change in the deformed shape.

Figures 16(a)–(c) present the time-dependent displacement along the Y-axis of a column under dynamic loading, captured at three different selected times (t = 1 s, t = 3263 s, and t = 10 000 s). The colour gradient represents the blue (lower displacement) to red (higher displacement), visually depicting the variation in displacement intensity, with red zones consistently indicating regions of maximum response.

Figures 17(a)–(c) present the time-dependent displacement along the Z-axis of a column under dynamic loading, captured at three different selected times (t = 1 s, t = 6415 s, and t = 10 000 s). The colour gradient represents the blue (lower displacement) to red (higher displacement), visually depicting the variation in displacement intensity, with red zones consistently indicating regions of maximum response.

Figures 18(a)–(c) show the first principal stress (at t = 1 s, t = 5443 s, and t = 10 000 s), and Figures 19(a)–(c) show the second principal stress (at t = 1 s, t = 6541 s, and t = 10 000 s). Notably, these are useful for understanding the distribution of stress on the faces of the column. Principal stresses indicate maximum stress, helping identify critical zones where failure may occur.

Figures 20(a)–(c) present the first principal stress (at t = 1 s, t = 5443 s, and t = 10 000 s). These are useful for understanding the distribution of stresses on the faces of the column. Principal stresses indicate maximum stresses, helping identify critical zones where failure may occur.

Figure 21(a) illustrates the damage state at 6880 s; at this moment, the entire surface affected by the fire exhibits the highest temperatures. Figure 21(b) shows a comparison between the real image of the damaged column and the results obtained through computational mechanics.

This study has proved the effectiveness of an integrated approach combining advanced experimental diagnostics with high-fidelity CFD and FE modelling for post-fire assessment of RC structures. The analysis of a fire-damaged warehouse revealed significant degradation in structural elements, particularly columns and pre-stressed beams, due to asymmetric thermal exposure and internal factors such as embedded downpipes. Non-destructive tests and microstructural analyses provided reliable benchmarks for temperature estimation, validating the numerical simulations. The coupled methodology not only enhanced understanding of the fire-induced damage mechanisms but also offered a robust framework for evaluating residual capacity and planning retrofitting interventions.

Thermal restraint played a critical role in the observed damage patterns and residual behaviour of the structural elements. The beams, which were partially shielded by the slab and fixed at their supports, experienced restricted thermal expansion, generating additional axial forces and bending moments that exacerbated concrete spalling and tendon exposure. Similarly, columns subjected to asymmetric heating exhibited thermal gradients across their sections, while surrounding framing elements limited lateral expansion. This restraint induced secondary stresses and curvature that accelerated material degradation and stiffness loss. These findings highlight that thermal restraint, often overlooked in simplified analyses, significantly influences the overall fire response and must be considered to achieve accurate post-fire safety assessments and reliable retrofitting strategies.

In conclusion, this paper contributes to performance-based fire engineering practices by demonstrating a robust and integrated methodology that combines detailed experimental diagnostics, advanced computational modelling, and material characterisation. The findings offer deeper insights into the thermal and mechanical behaviour of fire-damaged RC structures, emphasising the need to account for thermal restraint and fire-induced degradation in post-fire assessments. This knowledge supports more informed decision making processes, enabling engineers to evaluate structural integrity more reliably and to design targeted, cost-effective interventions. Ultimately, this approach promotes safer and more resilient reconstruction strategies, enhances the sustainability of repair measures, and provides a practical foundation for future research and engineering guidelines focused on improving the fire performance of similar structural systems.

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Data & Figures

Figure 1.
Diagrams a and b illustrate cross sections with geo mortar layers and dimensions for monolithic consolidation, showing structural details and labelled measurements.The image contains two diagrams labeled a and b, depicting original cross sections for geo mortar used in monolithic consolidation. Diagram a features a T shaped cross section marked with various spatial measurements along the top and bottom, including specific metrics such as zero point zero two, zero point zero five, and zero point eight zero. Each segment and layer is denoted clearly, with a layer of micro cords detailed in dotted lines. Diagram b presents a more complex shape with various labeled measurements such as two point five six and zero point eight three, illustrating how the geo mortar is applied for consolidation, including annotations that indicate layering. The layout displays a systematic presentation with key information emphasizing the structural dimensions necessary for the application of geo mortar.

The load-bearing structures: (a) rectangular pre-stressed concrete beams of type TR and (b) ribbed ‘omega’ beams

Figure 1.
Diagrams a and b illustrate cross sections with geo mortar layers and dimensions for monolithic consolidation, showing structural details and labelled measurements.The image contains two diagrams labeled a and b, depicting original cross sections for geo mortar used in monolithic consolidation. Diagram a features a T shaped cross section marked with various spatial measurements along the top and bottom, including specific metrics such as zero point zero two, zero point zero five, and zero point eight zero. Each segment and layer is denoted clearly, with a layer of micro cords detailed in dotted lines. Diagram b presents a more complex shape with various labeled measurements such as two point five six and zero point eight three, illustrating how the geo mortar is applied for consolidation, including annotations that indicate layering. The layout displays a systematic presentation with key information emphasizing the structural dimensions necessary for the application of geo mortar.

The load-bearing structures: (a) rectangular pre-stressed concrete beams of type TR and (b) ribbed ‘omega’ beams

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Figure 2.
Diagram depicting a load-bearing beam and a roofing element with dimensions labeled, showing their sizes and shapes.The image displays two technical sketches. Part a features a load bearing beam with dimensions of zero point seven four metres in width and eleven point eight metres in height, illustrated with diagonal lines and labeled appropriately. Part b presents a covering or roofing element, type A L I A N T dash 2, with a maximum width of two point four metres, a height of zero point eight four metres, and a length of one hundred ninety one point zero metres. The roofing element is shown with a smooth curve. Each section includes dimension lines indicating the measurements clearly and accurately while maintaining a straightforward presentation of technical details.

(a) TH 120 beam and (b) covering element of type Aliant 2

Figure 2.
Diagram depicting a load-bearing beam and a roofing element with dimensions labeled, showing their sizes and shapes.The image displays two technical sketches. Part a features a load bearing beam with dimensions of zero point seven four metres in width and eleven point eight metres in height, illustrated with diagonal lines and labeled appropriately. Part b presents a covering or roofing element, type A L I A N T dash 2, with a maximum width of two point four metres, a height of zero point eight four metres, and a length of one hundred ninety one point zero metres. The roofing element is shown with a smooth curve. Each section includes dimension lines indicating the measurements clearly and accurately while maintaining a straightforward presentation of technical details.

(a) TH 120 beam and (b) covering element of type Aliant 2

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Figure 3.
Exterior and interior views of a damaged building show fire effects and debris inside.The image presents two views of a severely damaged building. The left side shows the exterior view of the structure, which features a partially burned side with debris scattered across the ground. The right side offers an interior view, revealing cracked walls and more debris, including twisted metal and materials that indicate structural damage. The overall condition suggests significant fire damage and neglect, with both sections highlighting the extent of destruction.

Warehouse: (a) outside view and (b) inside view

Figure 3.
Exterior and interior views of a damaged building show fire effects and debris inside.The image presents two views of a severely damaged building. The left side shows the exterior view of the structure, which features a partially burned side with debris scattered across the ground. The right side offers an interior view, revealing cracked walls and more debris, including twisted metal and materials that indicate structural damage. The overall condition suggests significant fire damage and neglect, with both sections highlighting the extent of destruction.

Warehouse: (a) outside view and (b) inside view

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Figure 4.
A building floor plan showing a designated fire zone highlighted in red, with dimensions labeled in metres and axis orientations for x, y, and z.The image depicts a building floor plan with a highlighted fire zone in red, occupying the central part of the layout. The top section of the image outlines the floor plan, displaying various rooms and labeled dimensions in metres, with measurements shown alongside the grid lines. The axis orientations for x and y are positioned on the left side, while the bottom section features a cross section view with the z axis orientation indicated. The structure includes support beams and other architectural features visible in the detailed drawing, with consistent use of measurements and annotations throughout the floor plan.

Primary fire-damaged area in the warehouse

Figure 4.
A building floor plan showing a designated fire zone highlighted in red, with dimensions labeled in metres and axis orientations for x, y, and z.The image depicts a building floor plan with a highlighted fire zone in red, occupying the central part of the layout. The top section of the image outlines the floor plan, displaying various rooms and labeled dimensions in metres, with measurements shown alongside the grid lines. The axis orientations for x and y are positioned on the left side, while the bottom section features a cross section view with the z axis orientation indicated. The structure includes support beams and other architectural features visible in the detailed drawing, with consistent use of measurements and annotations throughout the floor plan.

Primary fire-damaged area in the warehouse

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Figure 5.
Three images showing damaged interiors with debris, structural elements, and walls in varying states of decay.The image consists of three sections labeled a, b, and c, depicting interiors of a damaged space. Each section illustrates chaotic environments filled with debris, such as scattered construction materials, remnants of furniture, and exposed structural elements. In section a, the view shows a large amount of debris covering the floor with visible structural pillars and a wall in decay. Section b focuses on a similar environment with more debris, including block like structures, revealing more about the interior's disrepair. Section c centers on a specific vertical structural column in significant distress, highlighting exposed materials and decay. Each section captures the extent of destruction and disarray in these interiors.

Damages inside the warehouse: (a) overview, (b) column, and (c) beam

Figure 5.
Three images showing damaged interiors with debris, structural elements, and walls in varying states of decay.The image consists of three sections labeled a, b, and c, depicting interiors of a damaged space. Each section illustrates chaotic environments filled with debris, such as scattered construction materials, remnants of furniture, and exposed structural elements. In section a, the view shows a large amount of debris covering the floor with visible structural pillars and a wall in decay. Section b focuses on a similar environment with more debris, including block like structures, revealing more about the interior's disrepair. Section c centers on a specific vertical structural column in significant distress, highlighting exposed materials and decay. Each section captures the extent of destruction and disarray in these interiors.

Damages inside the warehouse: (a) overview, (b) column, and (c) beam

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Figure 6.
Architectural floor plan showing multiple sections labeled with letters and numbers for identification.Detailed architectural floor plan layout depicting various sections segmented into identified areas. Sections are categorized with both letter and number labels, indicating different spaces such as rooms or facilities. The layout is organized with vertical and horizontal lines demarcating walls and rooms, while circular and rectangular labels highlight specific locations. Elements such as the green ovals labelled T and yellow circles labelled L signify different room types or functional areas. The numbering system assists in navigation, with main sections designated in a grid like pattern. The overall structure provides clear spatial relationships among the components.

Plan view of the fire zone. T-shaped transversal beam are labelled with ‘T’, while omega-shaped longitudinal beam are labelled with ‘L’

Figure 6.
Architectural floor plan showing multiple sections labeled with letters and numbers for identification.Detailed architectural floor plan layout depicting various sections segmented into identified areas. Sections are categorized with both letter and number labels, indicating different spaces such as rooms or facilities. The layout is organized with vertical and horizontal lines demarcating walls and rooms, while circular and rectangular labels highlight specific locations. Elements such as the green ovals labelled T and yellow circles labelled L signify different room types or functional areas. The numbering system assists in navigation, with main sections designated in a grid like pattern. The overall structure provides clear spatial relationships among the components.

Plan view of the fire zone. T-shaped transversal beam are labelled with ‘T’, while omega-shaped longitudinal beam are labelled with ‘L’

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Figure 7.
 A 3 D model depicting a building structure with various colored sections, representing different areas, alongside axes labeled x, y, and z for orientation.The image features a three dimensional model of a building structure, showcasing an intricate layout with sections in various colours, illustrating distinct areas within the building. The model is rendered in vibrant hues including blue, green, and red, which represent different regions or functions within the space. At the lower right corner, coordinate axes are displayed, labeled as x, y, and z, providing a spatial orientation for understanding the dimensions of the model. The overall structure appears complex, with multiple enclosed and open spaces denoting possible room configurations or purposes.

CFD model of the fire zone

Figure 7.
 A 3 D model depicting a building structure with various colored sections, representing different areas, alongside axes labeled x, y, and z for orientation.The image features a three dimensional model of a building structure, showcasing an intricate layout with sections in various colours, illustrating distinct areas within the building. The model is rendered in vibrant hues including blue, green, and red, which represent different regions or functions within the space. At the lower right corner, coordinate axes are displayed, labeled as x, y, and z, providing a spatial orientation for understanding the dimensions of the model. The overall structure appears complex, with multiple enclosed and open spaces denoting possible room configurations or purposes.

CFD model of the fire zone

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Figure 8.
Line graph displaying H R R P U A in kilowatts per square meter against time in minutes, showing a peak around 1,400 minutes and a gradual decline thereafter.The graph illustrates the relationship between H R R P U A, measured in kilowatts per square metre, plotted against time in minutes. The vertical axis indicates H R R P U A values ranging from zero to five thousand kilowatts per square metre, while the horizontal axis represents time, spanning from zero to three thousand five hundred minutes. A prominent peak is observed around one thousand four hundred minutes, followed by a gradual decline in H R R P U A values as time progresses, reflecting changes over the specified duration. The line is continuous and smooth, indicating a flowing trend without abrupt movements or discontinuities.

HRRPUA curve

Figure 8.
Line graph displaying H R R P U A in kilowatts per square meter against time in minutes, showing a peak around 1,400 minutes and a gradual decline thereafter.The graph illustrates the relationship between H R R P U A, measured in kilowatts per square metre, plotted against time in minutes. The vertical axis indicates H R R P U A values ranging from zero to five thousand kilowatts per square metre, while the horizontal axis represents time, spanning from zero to three thousand five hundred minutes. A prominent peak is observed around one thousand four hundred minutes, followed by a gradual decline in H R R P U A values as time progresses, reflecting changes over the specified duration. The line is continuous and smooth, indicating a flowing trend without abrupt movements or discontinuities.

HRRPUA curve

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Figure 9.
This graph depicts temperature in degrees Celsius over time in minutes, showing fluctuations in temperature values.The graph illustrates the relationship between temperature in degrees Celsius and time in minutes. The vertical axis represents temperature, ranging from zero to one thousand degrees Celsius, marked at intervals of two hundred degrees. The horizontal axis indicates time from zero to two hundred fifty minutes, with increments marked at intervals of fifty minutes. The temperature values fluctuate significantly, with a distinct peak observed early in the time period. The data line is presented in a thick red format, highlighting the temperature changes over time.

The average temperature–time diagram (CFD model)

Figure 9.
This graph depicts temperature in degrees Celsius over time in minutes, showing fluctuations in temperature values.The graph illustrates the relationship between temperature in degrees Celsius and time in minutes. The vertical axis represents temperature, ranging from zero to one thousand degrees Celsius, marked at intervals of two hundred degrees. The horizontal axis indicates time from zero to two hundred fifty minutes, with increments marked at intervals of fifty minutes. The temperature values fluctuate significantly, with a distinct peak observed early in the time period. The data line is presented in a thick red format, highlighting the temperature changes over time.

The average temperature–time diagram (CFD model)

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Figure 10.
A series of four 3 D models showing different perspectives of a building layout with directional axes indicated.The image displays four 3 D models, labelled a to d, of a building's layout viewed from various angles. In the top left, model a shows a front view with a y axis and an x axis indicated on the left. Model b, to the right, presents an angled perspective of the building's interior. The bottom left features model c from a different angle, while model d on the right highlights a tilted view with a directional x, y, and z axis indicated. The models utilise various colours to represent different elements within the building.

CFD model of the fire developing in the compartment at (a) t = 15 min, (b) t = 25 min, (c) t = 90 min, and (d) t = 1000 min

Figure 10.
A series of four 3 D models showing different perspectives of a building layout with directional axes indicated.The image displays four 3 D models, labelled a to d, of a building's layout viewed from various angles. In the top left, model a shows a front view with a y axis and an x axis indicated on the left. Model b, to the right, presents an angled perspective of the building's interior. The bottom left features model c from a different angle, while model d on the right highlights a tilted view with a directional x, y, and z axis indicated. The models utilise various colours to represent different elements within the building.

CFD model of the fire developing in the compartment at (a) t = 15 min, (b) t = 25 min, (c) t = 90 min, and (d) t = 1000 min

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Figure 11.
Temperature plot with gradient colours indicating varying heat levels over a surface, alongside metadata including file reference, node count, element count, and time duration.The image displays a temperature plot with a gradient of colours representing different heat levels across a surface. The uppermost area is shown in red, indicating high temperatures, and transitions to blue at the lowest temp range. In the top right corner, metadata includes the file reference Diamond 2012 dot a dot 0 for S A F I R, total nodes listed as four thousand five hundred eighty eight, total elements as four thousand four hundred fifty three, and a time duration of ten thousand seconds. Different temperature values, ranging from twenty three point five degrees to six hundred thirteen point ten degrees, are labelled next to corresponding colour bands, providing insight into the temperature distribution across the surface.

Finite element temperature distribution in the cross-section of Column 5

Figure 11.
Temperature plot with gradient colours indicating varying heat levels over a surface, alongside metadata including file reference, node count, element count, and time duration.The image displays a temperature plot with a gradient of colours representing different heat levels across a surface. The uppermost area is shown in red, indicating high temperatures, and transitions to blue at the lowest temp range. In the top right corner, metadata includes the file reference Diamond 2012 dot a dot 0 for S A F I R, total nodes listed as four thousand five hundred eighty eight, total elements as four thousand four hundred fifty three, and a time duration of ten thousand seconds. Different temperature values, ranging from twenty three point five degrees to six hundred thirteen point ten degrees, are labelled next to corresponding colour bands, providing insight into the temperature distribution across the surface.

Finite element temperature distribution in the cross-section of Column 5

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Figure 12.
Contour plot illustrating temperature distribution over a specified time, showing a gradient from warm to cooler areas, represented by colour bands.Contour plot displaying temperature distribution, labelled as Diamond 2012 dot a dot 0 for S A F I R with a time frame of 10,000 seconds. The plot features colour bands indicating temperature ranges from a high of 483.30 to a low of 23.00 degrees. The temperature gradients vary from red for the highest temperatures at the top to blue for the lowest at the bottom. The layout includes nodes and elements, with a designation of 6858 nodes and 6394 elements, highlighting a specific cross section denoted as Trave underscore T underscore sezione 4. Boxed areas near temperature markings indicate measurement points within the contour. The arrangement flows primarily from top to bottom and left to right, outlining variations across the plot.

Max. temperature distribution of beam T5 midspan cross-section

Figure 12.
Contour plot illustrating temperature distribution over a specified time, showing a gradient from warm to cooler areas, represented by colour bands.Contour plot displaying temperature distribution, labelled as Diamond 2012 dot a dot 0 for S A F I R with a time frame of 10,000 seconds. The plot features colour bands indicating temperature ranges from a high of 483.30 to a low of 23.00 degrees. The temperature gradients vary from red for the highest temperatures at the top to blue for the lowest at the bottom. The layout includes nodes and elements, with a designation of 6858 nodes and 6394 elements, highlighting a specific cross section denoted as Trave underscore T underscore sezione 4. Boxed areas near temperature markings indicate measurement points within the contour. The arrangement flows primarily from top to bottom and left to right, outlining variations across the plot.

Max. temperature distribution of beam T5 midspan cross-section

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Figure 13.
A wall reveals exposed concrete along with steel rebar, showing signs of damage and wear from previous repairs and weathering."The image depicts a section of a wall that has deteriorated, revealing exposed concrete with visible steel rebar embedded within it. The surrounding area shows peeling paint and crumbling plaster, indicating wear, damage, or previous renovations. Various textures from the concrete and bricks are noticeable, with uneven surfaces characteristic of ageing materials. The overall structure illustrates a sense of neglect or the need for repair. Additionally, electrical wiring can be seen hanging above the wall."

Column 6 damages

Figure 13.
A wall reveals exposed concrete along with steel rebar, showing signs of damage and wear from previous repairs and weathering."The image depicts a section of a wall that has deteriorated, revealing exposed concrete with visible steel rebar embedded within it. The surrounding area shows peeling paint and crumbling plaster, indicating wear, damage, or previous renovations. Various textures from the concrete and bricks are noticeable, with uneven surfaces characteristic of ageing materials. The overall structure illustrates a sense of neglect or the need for repair. Additionally, electrical wiring can be seen hanging above the wall."

Column 6 damages

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Figure 14.
Three visualisations show nodal temperature solutions at different steps in a simulation, featuring varying temperature ranges indicated by colour gradients and fluid flow patterns.The image contains three visualisations labeled a, b, and c displaying nodal temperature solutions from a simulation across different steps. Each visualisation includes a 3 D representation of fluid flow with a circular feature in the centre, indicating temperature distribution. The respective annotations indicate the step, substep, time, average temperature, and minimum and maximum temperature values. The temperature ranges are colour coded with gradations reflecting different values, and the colour bar below each visualisation provides a scale for interpreting these temperature values, varying from minimum to maximum across the different steps in the simulation. Each visualisation shows distinct temperature distributions, with a consistent layout including axes denoted as X, Y, and Z. The flow of data is presented from left to right and top to bottom, facilitating interpretation across the visualisations.

Temperature distribution at (a) t = 455 s, (b) t = 6415 s, and (c) t = 10 000 s

Figure 14.
Three visualisations show nodal temperature solutions at different steps in a simulation, featuring varying temperature ranges indicated by colour gradients and fluid flow patterns.The image contains three visualisations labeled a, b, and c displaying nodal temperature solutions from a simulation across different steps. Each visualisation includes a 3 D representation of fluid flow with a circular feature in the centre, indicating temperature distribution. The respective annotations indicate the step, substep, time, average temperature, and minimum and maximum temperature values. The temperature ranges are colour coded with gradations reflecting different values, and the colour bar below each visualisation provides a scale for interpreting these temperature values, varying from minimum to maximum across the different steps in the simulation. Each visualisation shows distinct temperature distributions, with a consistent layout including axes denoted as X, Y, and Z. The flow of data is presented from left to right and top to bottom, facilitating interpretation across the visualisations.

Temperature distribution at (a) t = 455 s, (b) t = 6415 s, and (c) t = 10 000 s

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Figure 15.
Three 3 D models showing displacement over varying steps in a simulated environment, with specific values for each model presented alongside them.The image depicts three 3 D models of displacement, labelled a, b, and c, showcasing how the structure changes at different simulation steps. Each section includes key information: the step number, sub iteration, time, and maximum displacement values. In model a, at step one, the maximum displacement D M X is zero point five three four times ten to the power of negative three. In model b, at step six, the D M X is zero point seven two four times ten to the power of negative three. In model c, at step twelve, the D M X is zero point zero one four one seven. Each model displays a vertical structure with a grid overlay, with arrows indicating axes in different colours for better visual comprehension.

Deformation at (a) t = 1 s, (b) t = 5443 s, and (c) t = 10 000 s

Figure 15.
Three 3 D models showing displacement over varying steps in a simulated environment, with specific values for each model presented alongside them.The image depicts three 3 D models of displacement, labelled a, b, and c, showcasing how the structure changes at different simulation steps. Each section includes key information: the step number, sub iteration, time, and maximum displacement values. In model a, at step one, the maximum displacement D M X is zero point five three four times ten to the power of negative three. In model b, at step six, the D M X is zero point seven two four times ten to the power of negative three. In model c, at step twelve, the D M X is zero point zero one four one seven. Each model displays a vertical structure with a grid overlay, with arrows indicating axes in different colours for better visual comprehension.

Deformation at (a) t = 1 s, (b) t = 5443 s, and (c) t = 10 000 s

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Figure 16.
 Three 3 D visualizations display a model showing nodal solutions with varying averages over different steps and subs at specified time points.The image presents three 3 D visualisations labelled a, b, and c, each illustrating a model with nodal solutions. Each visualisation includes data related to different steps, subs, and time points. In the left visualisation a, the step is one with an average displacement labelled as U Y, showing values for R S Y S, D M X, and S M N. The middle visualisation b corresponds to step five, with updated values for U Y, R S Y S, D M X, S M N, and S M X. The right visualisation c signifies step twelve, sharing a similar format to the others, including values for U Y, R S Y S, D M X, S M N, and S M X. Each visualisation has a corresponding colour scale at the bottom, which represents the range of values shown. The axis labels indicate the orientation of the model, with arrows pointing out the X, Y, and Z axes. The models are depicted in a gradient of colours, reflecting the variation in data across different configurations.

Displacement in the y-direction at (a) t = 1 s, (b) t = 3263 s, and (c) t = 10 000 s

Figure 16.
 Three 3 D visualizations display a model showing nodal solutions with varying averages over different steps and subs at specified time points.The image presents three 3 D visualisations labelled a, b, and c, each illustrating a model with nodal solutions. Each visualisation includes data related to different steps, subs, and time points. In the left visualisation a, the step is one with an average displacement labelled as U Y, showing values for R S Y S, D M X, and S M N. The middle visualisation b corresponds to step five, with updated values for U Y, R S Y S, D M X, S M N, and S M X. The right visualisation c signifies step twelve, sharing a similar format to the others, including values for U Y, R S Y S, D M X, S M N, and S M X. Each visualisation has a corresponding colour scale at the bottom, which represents the range of values shown. The axis labels indicate the orientation of the model, with arrows pointing out the X, Y, and Z axes. The models are depicted in a gradient of colours, reflecting the variation in data across different configurations.

Displacement in the y-direction at (a) t = 1 s, (b) t = 3263 s, and (c) t = 10 000 s

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Figure 17.
Three thermal analysis visualizations show different stages of a model's nodal solution, including variable data like R S Y S, D M X, S M N, and S M X for each step displayed.The image presents three separate thermal analysis visualisations of a model, denoted as a, b, and c. Each visualisation features a distinct nodal solution with accompanying variable data. Each section lists parameters such as STEP, SUB, TIME, and a variable U Z, average. Additionally, R S Y S, D M X, S M N, and S M X values are provided for each step, capturing changes across different analysis phases. Each visualisation likely contains colour gradients representing thermal distributions, though specific colours are not mentioned. The layouts suggest a consistent format across the three segments, facilitating comparative analysis of the model's thermal behaviour over time.

Displacement in the z-direction at (a) t = 1 s, (b) t = 6415 s, and (c) t = 10 000 s

Figure 17.
Three thermal analysis visualizations show different stages of a model's nodal solution, including variable data like R S Y S, D M X, S M N, and S M X for each step displayed.The image presents three separate thermal analysis visualisations of a model, denoted as a, b, and c. Each visualisation features a distinct nodal solution with accompanying variable data. Each section lists parameters such as STEP, SUB, TIME, and a variable U Z, average. Additionally, R S Y S, D M X, S M N, and S M X values are provided for each step, capturing changes across different analysis phases. Each visualisation likely contains colour gradients representing thermal distributions, though specific colours are not mentioned. The layouts suggest a consistent format across the three segments, facilitating comparative analysis of the model's thermal behaviour over time.

Displacement in the z-direction at (a) t = 1 s, (b) t = 6415 s, and (c) t = 10 000 s

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Figure 18.
Three visualizations depicting a nodal solution at different steps, showing a model with stress values and annotations indicating minimum and maximum points.The image displays three distinct visualisations labelled a, b, and c, each showing a vertical model representing a nodal solution at different analytical steps. The details for each visualisation include step number, sub, time, and average stress values. The model features annotations indicating maximum and minimum stress points marked as M X and M N, respectively. Each frame includes a colour gradient scale below, illustrating the range of stress values from a minimum to a maximum value at each step. The data presented in the visualisations shows variations in stress distribution across the model during various analysis stages, highlighting important stress metrics.

First principal stress at (a) t = 1 s, (b) t = 5443 s, and (c) t = 10 000 s

Figure 18.
Three visualizations depicting a nodal solution at different steps, showing a model with stress values and annotations indicating minimum and maximum points.The image displays three distinct visualisations labelled a, b, and c, each showing a vertical model representing a nodal solution at different analytical steps. The details for each visualisation include step number, sub, time, and average stress values. The model features annotations indicating maximum and minimum stress points marked as M X and M N, respectively. Each frame includes a colour gradient scale below, illustrating the range of stress values from a minimum to a maximum value at each step. The data presented in the visualisations shows variations in stress distribution across the model during various analysis stages, highlighting important stress metrics.

First principal stress at (a) t = 1 s, (b) t = 5443 s, and (c) t = 10 000 s

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Figure 19.
Three computational fluid dynamics visualizations display varying nodal solutions with data values for different steps and averages.The image displays three computational fluid dynamics visualisations labeled a, b, and c representing nodal solutions with varying parameters. Each visualisation shows a three dimensional structure with corresponding data extracted from simulation steps, including STEP, SUB, TIME, and average values for S 2. Specific values are indicated for D M X, S M N, and S M X across each visualisation, denoting the maximum and minimum values. The visual representations are accompanied by gradient colour bars indicating data variation, supporting contextual understanding of the simulations. Each section features a coordinate axis indicator, demonstrating the orientation of the results.

Second principal stress at (a) t = 1 s, (b) t = 6541 s, and (c) t = 10 000 s

Figure 19.
Three computational fluid dynamics visualizations display varying nodal solutions with data values for different steps and averages.The image displays three computational fluid dynamics visualisations labeled a, b, and c representing nodal solutions with varying parameters. Each visualisation shows a three dimensional structure with corresponding data extracted from simulation steps, including STEP, SUB, TIME, and average values for S 2. Specific values are indicated for D M X, S M N, and S M X across each visualisation, denoting the maximum and minimum values. The visual representations are accompanied by gradient colour bars indicating data variation, supporting contextual understanding of the simulations. Each section features a coordinate axis indicator, demonstrating the orientation of the results.

Second principal stress at (a) t = 1 s, (b) t = 6541 s, and (c) t = 10 000 s

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Figure 20.
Three graphical representations showing nodal solutions with various steps, times, and average values for parameters like D M X, S M N, and S M X.The image displays three separate graphical representations labelled a, b, and c, each illustrating nodal solutions from a simulation. Each representation features a vertical structure with numerical values indicating parameters relevant to the simulation at different time steps and subsystems. The leftmost graphic corresponds to STEP one with parameters such as D M X equal to negative five hundred thirty four thousandths, S M N approximately negative thirty million four hundred thousandths, and S M X around negative nineteen million two hundred thousandths. The middle graphic shows STEP six with D M X at negative seven hundred twenty four thousandths, S M N at approximately negative one hundred forty nine million eight hundred thousandths, and S M X as one hundred ninety seven thousand seven hundred forty nine. The rightmost graphic represents STEP twelve with D M X equal to 0.01417, S M N at approximately negative four hundred fifty seven million, and S M X at five hundred thirty four thousand two hundred two. A scale at the bottom of each graphic indicates the range of values. Each graphic has consistent labelling and a similar visual format, allowing for comparison across steps.

Third principal stress at (a) t = 1 s, (b) t = 5443 s, and (c) t = 10 000 s

Figure 20.
Three graphical representations showing nodal solutions with various steps, times, and average values for parameters like D M X, S M N, and S M X.The image displays three separate graphical representations labelled a, b, and c, each illustrating nodal solutions from a simulation. Each representation features a vertical structure with numerical values indicating parameters relevant to the simulation at different time steps and subsystems. The leftmost graphic corresponds to STEP one with parameters such as D M X equal to negative five hundred thirty four thousandths, S M N approximately negative thirty million four hundred thousandths, and S M X around negative nineteen million two hundred thousandths. The middle graphic shows STEP six with D M X at negative seven hundred twenty four thousandths, S M N at approximately negative one hundred forty nine million eight hundred thousandths, and S M X as one hundred ninety seven thousand seven hundred forty nine. The rightmost graphic represents STEP twelve with D M X equal to 0.01417, S M N at approximately negative four hundred fifty seven million, and S M X at five hundred thirty four thousand two hundred two. A scale at the bottom of each graphic indicates the range of values. Each graphic has consistent labelling and a similar visual format, allowing for comparison across steps.

Third principal stress at (a) t = 1 s, (b) t = 5443 s, and (c) t = 10 000 s

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Figure 21.
Diagrams and a photograph of structural designs show various sections of a tall, grid-like structure, identifying different sections and reinforcing details.The image consists of multiple components related to structural engineering. On the left, several diagrams display a tall structure divided into sections, labelled as Sezione 1, Sezione 2, and Sezione 3. Each section features a grid layout with circular openings and various notations illustrating reinforcing materials. The middle section presents a photograph of a structural wall showcasing the exterior of a rebar framework amidst construction. On the right, there are additional diagrams that depict the grid structure from different angles, maintaining the same style and notations as the first set of diagrams. Each component focuses on various structural aspects and reinforcement details critical for analysis.

(a) Damage at 6880 s, and (b) comparison of the damage

Figure 21.
Diagrams and a photograph of structural designs show various sections of a tall, grid-like structure, identifying different sections and reinforcing details.The image consists of multiple components related to structural engineering. On the left, several diagrams display a tall structure divided into sections, labelled as Sezione 1, Sezione 2, and Sezione 3. Each section features a grid layout with circular openings and various notations illustrating reinforcing materials. The middle section presents a photograph of a structural wall showcasing the exterior of a rebar framework amidst construction. On the right, there are additional diagrams that depict the grid structure from different angles, maintaining the same style and notations as the first set of diagrams. Each component focuses on various structural aspects and reinforcement details critical for analysis.

(a) Damage at 6880 s, and (b) comparison of the damage

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Table 1.

Key findings of non-destructive tests (Stochino et al., 2017b)

MethodPurposeKey findings
X-ray diffraction (XRD)Identify mineralogical changes
  • Undamaged: Calcite, dolomite, portlandite, ettringite present

 
  • Fire-damaged: Absence of portlandite (>500°C), formation of perovskite, spurrite

 
  • Decarbonation of calcite/dolomite (∼700°C–900°C)

DTA and thermogravimetry (TG)Track thermal decomposition and estimate temperature
  • Undamaged: Peaks at ∼120°C (water), ∼500°C (portlandite), ∼750°C–950°C (carbonate decomposition)

 
  • Damaged: Loss of portlandite peak, high-temp decarbonation (∼880°C), shifted dehydroxylation onset

Optical microscopy (OM)Assess microstructural damage and colour change
  • Undamaged: Compact, intact transition zone

 
  • Damaged: Microcracks (20–40 µm), reddening at 300°C–350°C, whitening at 600°C–900°C, surface pulverisation (>700°C)

Scanning electron microscopy (SEM)High-resolution imaging of microstructure
  • Undamaged: Dense CSH, visible ettringite, no interfacial cracks

 
  • Damaged: Globular phases (melting), microcracks, aggregate-paste detachment, CSH degradation (>300°C)

Table 2.

Colorimetric results (L*, a*, and b*) and mineralogical phases detected on samples collected in situ

Sample seriesSub-sampleDepth: cmMineralogical phasesL*a*b*Colour target
Undamaged0E, Cal, Dol, P62.080.032.72CM
COL 4A−a0.5Cal, Dol, P*75.35−0.615.25CM
 −b1.5Cal, Dol73.450.274.01CM
 −c2.5Cal, Dol, P61.230.474.35CM
 −d4.5Cal, Dol, P58.363.675.18PBA
 −e7.5Cal, Dol, P54.635.286.43PBA
COL 5A−16Cal, Dol, P61.840.854.35CM
 −28Cal, Dol, P55.495.266.25PBA
COL 5B−10.5Cal, Dol, P70.550.214.25CM
 −22Cal, Dol, P61.780.863.58CM
 −32.7–4.5Cal, Dol, P55.495.136.43PBA
COL 8A−13Cal, Dol, P61.450.984.74CM
 −25Cal, Dol, P57.545.366.42PBA
COL 8B0.5Cal, Dol, P55.495.86.62PBA
COL 9A9.7Cal, Dol, P57.44.256.47PBA
COL 9B7.8Cal, Dol, P55.124.845.98PBA

COL, column; Cal, calcite; CM, cement matrix; Dol, dolomite; E, ettringite; P, portlandite; P*, relict or secondary portlandite; PBA, pinkish-beige aggregates

Table 3.

Synthesis of maximum temperature estimation detected on samples collected in situ

Sample seriesEst. max temp: °C
Undamaged20
COL 4A≈700
 >500
 ≤500
 <500–400
 400–300
COL 5A≤500
 400–300
COL 5B>500
 ≤500–400
 400–300
COL 8A≤500
 400–300
COL 8B
COL 9A400–300
COL 9B400–300

COL, column

Table 4.

Various materials and their burning characteristics

Material categoryDensity: kg/m³Thickness: mThermal conductivity:
W/m·K
Specific heat
capacity:
kJ/kg·K
Heat release
rate per unit
area: kW/m²
Ignition threshold: °C
Textiles (Clothes)5610.0250.1130.518391.4296
Synthetic Rubber (SBR)11000.020.171.881980.97390
Cellulose (Paper)9300.0070.181.341.561230
Thermoplastic (PP)9000.0060.386.31782.44210
Polymer Blend (PE-PP)9150.0080.383.45273309
Construction (Drywall)8000.0130.28408230
Metal (Steel)79000.0114.90.477131.91400
Storage (Shelving)79000.0070.140.471255.44400
Electrical (Panel)89200.1233900.385429.775300
Composite (Steel + Paper)23240.01714.90.477432.811230
Composite (Steel + Plastic)23120.01714.90.47755.697210
Packaging (PET Pallets)6000.10.122.723811.294210
Table 5.

A comparative analysis of the maximum temperatures forecasted by the numerical model

Column numberHeight: mExp. max temp: °CCFD max temp: °CDifference: %
5 b4.73>50061322%
5 a1.0650072244%
71.555005326%
9 a4.365005061%
9 b0.9850038423%
Beam Number    
5–65.9830–8608015%
8–95.950056513%
9–106.7820–9208364%

COL, column; Cal, calcite; CM, cement matrix; Dol, dolomite; E, ettringite; P, portlandite; P*, relict or secondary portlandite; PBA, pinkish-beige aggregates

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