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- W865351437 abstract "This paper delineates the requirements and analysis procedure of the damage tolerance analysis for the aircraft safety and structural life prediction. The U.S. military specification (MIL-A-83444) describes the damage tolerance analysis requirements in terms of initial crack assumption, residual strength standard, and inspection periods, etc. Those are applied in appropriate manner in accordance with the structure types and inspectabilities. In this paper, damage tolerance analysis procedures according to the structure types and inspectabilities are briefly summarized. A damage tolerance analysis result of a small aircraft is also shown as an example." @default.
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- W865351437 date "1997-01-01" @default.
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- W865351437 title "The Damage Tolerance Analysis Techniques of an Aircraft Wing" @default.
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