Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
By: John W. Edwards.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 110284.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1996
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Transonic flutter; Transonic flow; Unsteady flow; Separated flow; Computational fluid dynamics; Flow equations; Mach number; Unsteady aerodynamics
Notes: Shipping list no.: 98-0599-M.

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