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
by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC, Springfield, Va
Written in English
|Other titles||EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996.|
|Statement||John W. Edwards.|
|Series||NASA-TM -- 110484., NASA technical memorandum -- 110484.|
|Contributions||Edwards, John W., United States. National Aeronautics and Space Administration.|
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