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Simulation Of Unsteady, Inviscid, Rotational, Transonic FlowReport describes numerical simulation of two-dimensional, unsteady, inviscid rotational, transonic flow about rigid airfoil in such motions as pitching or plunging oscillations. Study demonstrates potential utility of computation in analyses of aeroelasticity of airfoils.
Document ID
19920000109
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Damodaran, Murali
(NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 15, 2013
Publication Date
February 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-12113
Accession Number
92B10109
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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