Structural Fatigue Considerations in the Design of Rotary-Wing Vehicles

680672

02/01/1968

Event
National Aeronautic and Space Engineering and Manufacturing Meeting
Authors Abstract
Content
This paper attempts to outline some of the major fatigue considerations in the design of rotary-wing vehicles. The safety and economic advantages of a “fail-safe” structure are emphasized. Fatigue considerations at both the preliminary and detail design stages are discussed. While the fatigue phenomenon is somewhat incompletely understood from an academic standpoint, it is shown how practical engineering understanding and progress have resulted from existing scientific knowledge. The importance of statistical effects is noted in regard to both manufacturer-controlled variables and operator-controlled variables. Areas of likely future progress are also pointed out.
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DOI
https://doi.org/10.4271/680672
Pages
13
Citation
SMITH, H., "Structural Fatigue Considerations in the Design of Rotary-Wing Vehicles," SAE Technical Paper 680672, 1968, https://doi.org/10.4271/680672.
Additional Details
Publisher
Published
Feb 1, 1968
Product Code
680672
Content Type
Technical Paper
Language
English