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Keywords: Fatigue
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Journal Articles
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 Chen et al. detected fretting patterns in self...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2022) 94 (2): 240–247.
Published: 29 November 2021
...), and strain level is identified. The study contributes to the theoretical aircraft maintenance literature and managers in practice. Ebru Yazgan can be contacted at: eyazgan@eskisehir.edu.tr Fatigue Aircraft maintenance technician Musculoskeletal disorders Ordinal logistics regression analysis...
Journal Articles
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
Aircraft Engineering and Aerospace Technology: An International Journal (2019) 91 (2): 235–240.
Published: 11 October 2018
... under the driven head and has a smaller thickness in this area. Wojciech Wronicz can be contacted at: wojciech.wronicz@ilot.edu.pl 15 01 2018 20 02 2018 01 03 2018 It is commonly accepted that compressive residual stresses increase fatigue life, as they delay crack...
Journal Articles
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
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
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
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
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
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
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
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
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
... 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 Hercules aircraft. A rig will be constructed, and housed in a purpose built hangar, to test...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2002) 74 (6)
Published: 01 December 2002
... The reason why such corrosion-induced fatigue failures seem endemic only in France is puzzling. Textron Lycoming had advanced a theory on climatic differences between France and the United States as one reason for the disparity in experience, but one would expect that any such adverse...
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
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
... © MCB UP Limited 1999 --> USF Impact Finishers Peening Aviation Fatigue Keywords USF Impact Finishers, Peening, Aviation,'Fatigue Surface finishing and impact treatment subcontractor, USF Impact Finishers,has published a new 12-page colour brochure detailing its...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (1999) 71 (5)
Published: 01 October 1999
... Keywords: Royal Aeronautical Society, Testing, Fatigue, Components,Aircraft, Risk assessment Continuing the theme of life extension was a paper from Rolls-Royce on the"Lifing of critical rotating parts: science or technology?", which began by stating a technological approach...
Journal Articles
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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