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1-20 of 25
Keywords: Fatigue
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Journal Articles
Investigation of microstructure of fretting wear behavior in 6061-T6 aluminum alloy
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Aircraft Engineering and Aerospace Technology: An International Journal (2023) 95 (8): 1194–1200.
Published: 25 April 2023
...@erciyes.edu.tr 02 11 2022 14 02 2023 21 03 2023 © Emerald Publishing Limited 2023 Emerald Publishing Limited Licensed re-use rights only Fretting wear Aluminum alloy Fatigue Aircraft structure Riveted lap joint The nominal composition of type 6061 aluminum is 0.25...
Journal Articles
A questionnaire-based musculoskeletal disorder assessment for aircraft maintenance technicians
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Aircraft Engineering and Aerospace Technology: An International Journal (2022) 94 (2): 240–247.
Published: 29 November 2021
... 09 05 2021 09 06 2021 20 07 2021 26 08 2021 © Emerald Publishing Limited 2021 Emerald Publishing Limited Licensed re-use rights only Fatigue Aircraft maintenance technician Musculoskeletal disorders Ordinal logistics regression analysis Aviation maintenance...
Journal Articles
Comparative fatigue properties estimation of composite structural nodes
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Aircraft Engineering and Aerospace Technology: An International Journal (2021) 93 (9): 1401–1411.
Published: 18 March 2021
...Miroslaw Rodzewicz Purpose The purpose of this paper is to present the concept of the author’s method of fatigue properties assessment of polymer composite structures, especially structures having nodes of concentrated force introduction (NCFI) using fatigue test data of coupons of similar...
Journal Articles
Application of computed tomography to hole expansion measurements
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Aircraft Engineering and Aerospace Technology: An International Journal (2019) 91 (2): 235–240.
Published: 11 October 2018
... 15 01 2018 20 02 2018 01 03 2018 © Emerald Publishing Limited 2018 Emerald Publishing Limited Licensed re-use rights only Fatigue Computed tomography Hole expansion Joints Rivet Fatigue properties are extremely important in aircraft design and exploitation...
Journal Articles
Fatigue life prediction of ceramic-matrix composites
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Aircraft Engineering and Aerospace Technology: An International Journal (2018) 90 (5): 720–726.
Published: 07 June 2018
...Longbiao Li Purpose This paper aims to predict fatigue life and fatigue limit of fiber-reinforced ceramic-matrix composites (CMCs) with different fiber preforms, i.e. unidirectional, cross-ply, 2D-, 2.5D- and 3D-woven, at room and elevated temperatures. Design/methodology/approach Under cyclic...
Journal Articles
Optimising the multiplicative AF model parameters for AA7075 cyclic plasticity and fatigue simulation
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Aircraft Engineering and Aerospace Technology: An International Journal (2018) 90 (2): 251–260.
Published: 05 March 2018
... The study uses a strain-life fatigue application to demonstrate the importance of incorporating a technique such as the presented multiobjective optimisation method to arrive at robust parameters capable of accurately simulating a variety of transient cyclic phenomena. Originality/value The proposed...
Journal Articles
A review on aircraft joints design
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Aircraft Engineering and Aerospace Technology: An International Journal (2016) 88 (3): 411–419.
Published: 03 May 2016
...Carlos Eduardo Chaves; Fernando Ferreira Fernandez Purpose The purpose of this paper is to present a review about sizing of joints, from the static and fatigue points of view. A discussion about advantages and disadvantages of each joining technology, among the ones mentioned above...
Journal Articles
Preliminary evaluation of the fatigue behaviour of aluminium alloy in corrosive environment
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Aircraft Engineering and Aerospace Technology: An International Journal (2015) 87 (2): 165–171.
Published: 02 March 2015
...Prof Richard Degenhardt, Dr Leslie J. Cohen; Giacomo Frulla; Gianni Avalle; Vito Sapienza Purpose – The purpose of this paper is to investigate the effect of fatigue life reduction of 2024 Al alloy for aerospace components due to the corrosive (exfoliation) environment. Both standard fatigue...
Journal Articles
Combined fatigue experiments on full scale turbine components
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Aircraft Engineering and Aerospace Technology: An International Journal (2013) 85 (1): 4–9.
Published: 18 January 2013
...Dianyin Hu; Rongqiao Wang Purpose The purpose of this paper is to perform experiments on a full scale turbine blade attached to a part of actual turbine disc at elevated temperature, which can accurately predict the life of a fir‐tree contact under high cycle fatigue (HCF)/low cycle fatigue (LCF...
Journal Articles
Fatigue crack detection in metallic plates with non‐linear Lamb wave modulation spectrum
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Aircraft Engineering and Aerospace Technology: An International Journal (2010) 82 (5): 279–283.
Published: 07 September 2010
...Gao Guili; Li Dayong; Shi Dequan; Dong Jingwei Purpose The purpose of this paper is to demonstrate by experiments that non‐linear Lamb wave modulation spectrum (NLWMS) will be a good indicator of fatigue cracks in a metallic plate. Design/methodology/approach A system composed of piezoelectric...
Journal Articles
Fatigue evaluation of high‐loaded aeronautical composite structures
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Aircraft Engineering and Aerospace Technology: An International Journal (2009) 81 (5): 452–460.
Published: 04 September 2009
...Mirosław Rodzewicz Purpose The purpose of this paper is to present a study on effective methods for fatigue evaluation of composite structures. Design/methodology/approach Based on topological correspondence between half‐cycle arrays and the Haig diagrams, the fatigue data for composite...
Journal Articles
Geometry factor determination of round specimens using fracture mechanic approaches in Al 2024‐T3
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Aircraft Engineering and Aerospace Technology: An International Journal (2007) 79 (5): 469–474.
Published: 11 September 2007
...Fuad M. Khoshnaw; Nazhad A. Hussain Purpose The purpose of the paper is to characterize the fatigue behavior, such as fatigue strength, and stress intensity factor values of aluminum alloy type 2024‐T3, using only a round specimen. The aim in this study is to interrelate the fatigue behavior...
Journal Articles
Analysis of transient temperature distribution
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Aircraft Engineering and Aerospace Technology: An International Journal (2004) 76 (6): 607–611.
Published: 01 December 2004
...Hai Li; Tao Cheng; Jin Zhang This paper focuses on investigation of a numerical method for transient temperature distribution, in order to analyze one kind of malfunction of turbine nozzle guide component of a turbo‐fan aeroengine. Thermal fatigue acts as the most important factor resulting...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2003) 75 (2)
Published: 01 April 2003
... © MCB UP Limited 2003 --> Marshall Aerospace Aircraft Fatigue Testing Keywords: Marshall Aerospace, Aircraft, Fatigue, Testing A contract awarded by the RAF C-130 IPT will see Marshall Aerospace undertaking a requirement to fatigue test the fuselage of a C-130 K...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2002) 74 (6)
Published: 01 December 2002
... © MCB UP Limited 2002 --> Aircraft Cylinders Engines Fatigue Fatigue in engine cylinder Keywords: Aircraft, Cylinders, Engines, Fatigue A student pilot in a single piston-engine Robin HR200/200B aircraft was on a solo cross-country navigation detail from...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2001) 73 (2)
Published: 01 April 2001
... © MCB UP Limited 2001 --> USA Military Fatigue Testing F-22 Program initiates fatigue testing Keywords USA, Military, Fatigue, Testing The F-22 program recently initiated the fatigue testing necessary to accomplish the next program milestone, according to US...
Journal Articles
Towards application of fibre metal laminates in large aircraft
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Aircraft Engineering and Aerospace Technology: An International Journal (1999) 71 (6): 558–570.
Published: 01 December 1999
...A. Vlot; L.B. Vogelesang; T.J. de Vries Fibre metal laminates were developed at Delft University during the last two decades as a family of new hybrid materials consisting of bonded thin metal sheets and fibre/adhesive layers. This laminated structure provides the material with excellent fatigue...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (1999) 71 (6)
Published: 01 December 1999
... in order to maximise performance. Details available from Christian Tyroll, USF Impact Finishers Ltd. Tel: +44(0)1753 526511; Fax: +44 (0)1753 538093. © MCB UP Limited 1999 --> USF Impact Finishers Peening Aviation Fatigue Keywords USF Impact Finishers, Peening, Aviation...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (1999) 71 (5)
Published: 01 October 1999
... © MCB UP Limited 1999 --> Royal Aeronautical Society Testing Fatigue Components Aircraft Risk assessment Royal Aeronautical Society/CEAS Forum - part 2 Keywords: Royal Aeronautical Society, Testing, Fatigue, Components,Aircraft, Risk assessment Continuing...
Journal Articles
Simulation driven design helps solve C5 cargo door problem
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Aircraft Engineering and Aerospace Technology: An International Journal (1999) 71 (4): 346–349.
Published: 01 August 1999
...Alan Pinnick Simulation driven design helped Lockheed Martin Aeronautical Systems solve a fatigue‐related problem on the cargo door of the C5 transport plane. Cracks in the area of the door’s upper hinge had led the Air Force to impose a special visual inspection of the door prior to each ADS...
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