Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
Subtitle: EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996
By: John W. Edwards.
Contributors: Edwards, John W.; United States. National Aeronautics and Space Administration.
Series: NASA-TM -- 110484.; NASA technical memorandum -- 110484.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Separated flow.; Transonic flow.; Transonic flutter.; Transonic speed.; Unsteady flow.; Viscous flow.; Computational fluid dynamics.; Coupling.; Airfoils.; Mach number.; Boundary layer separation.; Airfoil oscillations.
Other titles: EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996.
Notes: Shipping list no.: 97-0681-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.