Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer
By: Abdelkader Frendi.
Contributors: Langley Research Center.
Series: NASA contractor report -- 201691.; NASA contractor report -- NASA CR-201691.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1997
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Pressure gradients.; Supersonic boundary layers.; Turbulent boundary layer.; Boundary layer thickness.; High frequencies.
Notes: Shipping list no.: 98-0848-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.