Publication Date:
2016-06-07
Description:
A summary of tests conducted on the Concorde aircraft nacelle structure is presented. The tests were conducted as a part of the structural development and certification program. The nacelle structural specimens are described. The problems associated with the intake testing and engine-bay and nozzle testing are discussed.
Keywords:
STRUCTURAL MECHANICS
Type:
NASA. Langley Res. Center Advanced Approaches to Fatigue Evaluations; p 649-665
Format:
application/pdf
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