3 edition of Evaluation of a composite sandwich fuselage side panel with damage and subjected to internal pressure found in the catalog.
Evaluation of a composite sandwich fuselage side panel with damage and subjected to internal pressure
1997 by Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English
|Statement||Marshall Rouse ... [et al.].|
|Series||NASA technical memorandum -- 110309.|
|Contributions||Langley Research Center.|
|The Physical Object|
|Number of Pages||18|
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