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

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Bibliographic Details
Author / Creator:	Edwards, John W., author.
Imprint:	[Washington, DC] : [National Aeronautics and Space Administration], [1996]
Description:	1 online resource (16 pages) : illustrations.
Language:	English
Series:	NASA-TM ; 110484 NASA technical memorandum ; 110484.
Subject:	Separated flow. Transonic flow. Transonic flutter. Transonic speed. Unsteady flow. Viscous flow. Computational fluid dynamics. Coupling. Airfoils. Mach number. Boundary layer separation. Airfoil oscillations. Aerofoils. Computational fluid dynamics. Mach number. Viscous flow.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/11288195

Hidden Bibliographic Details
Other authors / contributors:	United States. National Aeronautics and Space Administration, issuing body.
Notes:	"EUROMECH-ColIoquium 349 Simulation of Fluid-Structure Interaction in Aeronautics, Gottingen, Germany, September 16-18, 1996." Includes bibliographical references (pages 15-16). Description based on online resource; title from PDF title page (NASA, viewed June 14, 2017).
Other form:	Microfiche version: Euromech Colloquium (349th : 1996 : Göttingen, Germany). Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
GPO item no.:	0830-D (online)
Govt.docs classification:	NAS 1.15:110484

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