Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method / John W. Edwards.

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Bibliographic Details
Online Access:	Online Access Online Access
Main Author:	Edwards, John W. (Author)
Format:	Government Document eBook
Language:	English
Published:	[Washington, DC] : [National Aeronautics and Space Administration], [1996]
Series:	NASA technical memorandum ; 110484.
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.

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Call Number:	NAS 1.15:110484
NAS 1.15:110484	Available