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

Bibliographic Details
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.
Online Access:	https://purl.fdlp.gov/GPO/gpo78886

Description
Item Description:	"EUROMECH-ColIoquium 349 Simulation of Fluid-Structure Interaction in Aeronautics, Gottingen, Germany, September 16-18, 1996."
Physical Description:	1 online resource (16 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 15-16).