Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
Subtitle: final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95
By: David S. Dolling and J.W. Barter.
Contributors: Barter, J. W.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-199334.
Publisher: 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
Published: 1995
Place of publication: Austin, Tex; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic loads.; Boundary layer control.; Boundary layer separation.; Corner flow.; Hypersonic boundary layer.; Shock wave interaction.; Turbulent boundary layer.; Unsteady flow.; Vortex generators.
Other titles: Control and reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0569-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1996] 1 microfiche.