Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces

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National Aeronautics and Space Administration, Dryden Flight Research Center, National Technical Information Service, distributor , Edwards, Calif, [Springfield, Va
Aerospace engineering, Sandwich structures, Debonding (Materials), Stress distribution, Curved panels, Structural engine
Other titlesOpen mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces.
StatementWilliam L. Ko.
SeriesNASA/TP -- 1999-206580., NASA technical paper -- 206580.
ContributionsNASA Dryden Flight Research Center.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL18137667M