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Saturday, May 2, 2020 | History

4 edition of Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method found in the catalog.

Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method

Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method

EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996

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Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC, Springfield, Va .
Written in English


Edition Notes

Other titlesEUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996.
StatementJohn W. Edwards.
SeriesNASA-TM -- 110484., NASA technical memorandum -- 110484.
ContributionsEdwards, John W., United States. National Aeronautics and Space Administration.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL17595884M
OCLC/WorldCa42671384


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Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method Download PDF EPUB FB2