The state of the art and the development history of aircraft structures reliability design are reviewed, partly as they are mirrored in official requirements, and partly as they are seen by workers in the field. Included are loading and stress calculations, aeroelasticity, dynamic response, the fatigue problem, and the utilization of composite materials are discussed.
The Changing Scene of Structural Airworthiness
1979
29 pages
Report
Keine Angabe
Englisch
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