Defining the Fatigue Load Environment for Business Aircraft

660215

02/01/1966

Event
2nd Annual Business Aircraft Conference
Authors Abstract
Content
Load environments for general aviation and business aircraft have not been a matter of concern in the past, except for static strength purposes. Increased recognition of the importance of fatigue qualification must be accompanied by an examination of how these aircraft are being used.
The approach suggested here is a simplification of that used by the transport aircraft industry. Examinations of the gust and maneuver load environments are made relative to different types of flight operations.
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Details
DOI
https://doi.org/10.4271/660215
Pages
11
Citation
Thompson, C., "Defining the Fatigue Load Environment for Business Aircraft," SAE Technical Paper 660215, 1966, https://doi.org/10.4271/660215.
Additional Details
Publisher
Published
Feb 1, 1966
Product Code
660215
Content Type
Technical Paper
Language
English