Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction [microform] : final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95 / David S. Dolling and J.W. Barter.

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Bibliographic Details
Main Author:	Dolling, David S.
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Barter, J. W.
Other title:	Control and reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction.
Format:	Government Document Microfilm Book
Language:	English
Published:	Austin, Tex. : [Washington, DC] : [Springfield, Va.] : Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], [1995]
Series:	NASA contractor report ; NASA CR-199334.
Subjects:	Aerodynamic loads. Boundary layer control. Boundary layer separation. Corner flow. Hypersonic boundary layer. Shock wave interaction. Turbulent boundary layer. Unsteady flow. Vortex generators.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:199334
NAS 1.26:199334	Restricted Place a Hold