... 2025 Emerald Publishing Limited Licensed re-use rights only CFD Modeling and simulation Finite element analysis Aerodynamics Flight safety The experimental methods used for the analysis of the aerodynamic properties of parachutes are: wind tunnel measurements and drop tests...

... loads. Another study demonstrated that optimizing a motor assembly bracket through finite element analysis (FEA) achieved a balance between weight and structural strength (Khan et al., 2022). These research efforts highlight the significance of FEA in predicting bracket performance, though...

...), subject to full attribution to the original publication and authors. The full terms of this licence maybe seen at Link to the terms of the CC BY 4.0 licence. Aeroelasticity Finite element analysis Optimization The category of small aircraft up to 600 kg maximum takeoff weight has...

... Heshmatollah Haghighat can be contacted at: hhaghighat@razi.ac.ir 25 10 2024 23 02 2025 04 03 2025 © Emerald Publishing Limited 2025 Emerald Publishing Limited Licensed re-use rights only Bimetal rod asymmetric rolling process Experiment Finite element analysis...

.... The variation of volume fraction of reinforcement particles (SiC) in a disk changes radially. Finite element analysis has been performed to investigate stress distribution in a layered disk. Findings The microstructural investigation was carried out under an optical microscope and scanning electron...

..., simple, economic and robust (LASER) project. After defining the requirements, the loads that the aircraft would be subjected to during its operation were defined from the flight envelope considering finite element analysis. The design vector consists of material choice for each laminate of the structure...

... form as: Finite element analysis Free vibration Bending Flexural analysis Skew sandwich structure Sandwich plate Skew angle Subrata Kumar Panda can be contacted at: pandask@nitrkl.ac.in 28 05 2016 19 04 2017 21 04 2017 © Emerald Publishing Limited 2018...

..., and final results for “maximum of all values” is shown. Structural analysis Finite element analysis Multibody analysis Thin-walled structures Transient dynamics The light aircraft parachute rescue system (PRS) that is subject to dynamic numerical analyses in this paper is nonstandard...

... in determining which properties need to be known to a high accuracy. Design of experiments Finite element analysis Carbon fiber composite Hashin Material properties In all cases, displacements were increased until a distinct maximum load was identified (i.e. damage had accrued to an extent...

... and transportation process. As platforms become smaller, deployable wing designs enable the concerned structures to be more effective by avoiding the volume restriction. (Jacob and Smith, 2009). Finite element analysis Shape memory polymer Aerodynamic loads Deployable morphing structure © Emerald...

... with the distributed load. Direct method was used to obtain the SIF values. FE mesh of the entire model and the cracks is shown in Figure 2 . Bonded composite repair structure Finite element analysis Multiple site damage Stress intensity factor Stress (materials) Materials Multiple sites damage...

... listed out in Table V . The aileron rotational stiffness provided in the initial design has been used for the finite element analysis and in general, the quality of an initial FE model of an aircraft is not guaranteed. This has resulted in a large variation in symmetric aileron rotational frequencies...

.... Giovanni Bernardini can be contacted at: g.bernardini@uniroma3.it © Emerald Group Publishing Limited 2012 Helicopters Computational geometry Finite element analysis Curved‐axis rotor blade Structural dynamics Aeroelasticity Finite‐element solution Rotary wings are complex systems...

..., undergo large amplitude nonlinear vibrations. Originality/value The paper will assist researchers of vibration behavior of elastic systems. © Emerald Group Publishing Limited 2008 Finite element analysis Vibration Shell structures An eight‐noded isoparametric element with five...

...=time Viktor Šajn can be contacted at: viktor.sajn@fs.uni‐lj.si © Emerald Group Publishing Limited 2007 Meshes Finite element analysis Compressible flow Rocket engines C_C=correction coefficient C_F=thrust coefficient...

... the stability behaviour of flying flexible rockets and missiles. © Emerald Group Publishing Limited 2006 Dynamics Finite element analysis The specifications of the beam taken into consideration : Weight of beam (dimensionless) 0.003 Figure 4 shows the plot of real and imaginary...

... that the maximum value is found also for ϕ=15°. Short shells of (0/90/0) laminate are found to provide decreasing nature in frequency parameters with increase in twist angle. Of course this trend is observed for both the laminates (0/90/0, 0/90) in case of intermediate shells. Finite element analysis...

...L. Ravi Kumar; P.K. Datta; D.L. Prabhakara Purpose To predict the critical flutter load and frequencies of doubly curved panels using first‐order shear deformation theory considering the effects of shear deformation and rotary inertia. Design/methodology/approach – A finite element analysis...

... of airfoils. © Emerald Group Publishing Limited 2004 Aerodynamics Finite element analysis Numerical analysis Simulation A_1…A₃=boundary e→=position vector of the variable boundary E=calculation domain in an element...

... component variants efficiently. © MCB UP Limited 2001 --> debis IT services Software Finite element analysis Pre and post-processing FEA software Keywords debis IT services, Software, Finite element analysis Medina, universal pre- and post-processing software developed...