Major sources of fatigue and continuous change of emphasis on different aspects of problem are considered with particular reference to some aircraft; principal fatigue items are usually wing tension-carrying members, and since most significant loads are those due to ground-to-air cycle and gusts, this part of structure is particularly sensitive to flight pattern; design criteria and factors in choice of materials; weight breakdown of structure of typical jet transport for different materials and alloy grades is also presented; manufacturing stage, development testing stage, and operational stage.
Designing to combat fatigue
Aircraft Eng
Aircraft Engineering ; 39 , n 10
1967
8 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Emerald Group Publishing | 1967
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