3 edition of Effect of adhesive interleaving and discontinuous plies on failure of composite laminates subject to transverse normal loads found in the catalog.
Effect of adhesive interleaving and discontinuous plies on failure of composite laminates subject to transverse normal loads
by National Aeronautics and Space Administration, Langley Research Center, For sale by the National Technical Information Service in Hampton, Va, [Springfield, Va
Written in English
|Statement||Dawn C. Jegley.|
|Series||NASA technical memorandum -- 101507.|
|Contributions||Langley Research Center.|
|The Physical Object|
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