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Journal Articles

The Fatigue Substantiation of the Lynx Helicopter

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A.D. Hall, BSc, CEng, MRAes
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1975) 47 (10): 4–17.
https://doi.org/10.1108/eb035277
Published: 01 October 1975
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Journal Articles

Fatigue Substantiation of Helicopter Components: The Part Played by Metal Fatigue in the Engineering of a Helicopter, the Methods Used to Estimate Safe Fatigue Lives of Helicopter Components, and the Results of Flight and Fatigue Testing with the Westland Wessex Helicopter

Available to Purchase
A.D. Hall, B.Sc.
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1963) 35 (11): 316–325.
https://doi.org/10.1108/eb033800
Published: 01 November 1963
View article titled, Fatigue Substantiation of Helicopter Components: The Part Played by Metal Fatigue in the Engineering of a Helicopter, the Methods Used to Estimate Safe Fatigue Lives of Helicopter Components, and the Results of Flight and Fatigue Testing with the Westland Wessex Helicopter
Open the PDF for Fatigue Substantiation of Helicopter Components: The Part Played by Metal Fatigue in the Engineering of a Helicopter, the Methods Used to Estimate Safe Fatigue Lives of Helicopter Components, and the Results of Flight and Fatigue Testing with the Westland Wessex Helicopter in another window
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Journal Articles

Assessing Helicopter Safety with Respect to Component Fatigue: A Procedure Based on Statistical Methods of Data Analysis Requiring a Catastrophic Failure Rate of less than I0–3 after 10,000 flying hours

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A.D. Hall, B.Sc.
Journal: Aircraft Engineering and Aerospace Technology
Aircraft Engineering (1963) 35 (4): 97–99.
https://doi.org/10.1108/eb033714
Published: 01 April 1963
View article titled, Assessing Helicopter Safety with Respect to Component Fatigue: A Procedure Based on Statistical Methods of Data Analysis Requiring a Catastrophic Failure Rate of less than I0–3 after 10,000 flying hours
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