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

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:
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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