Effect of density gradients in confined supersonic shear layers
By: Oshin Peroomian and R.E. Kelly.
Contributors: Kelly, R. E.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-198029 - NASA CR-198030.; NASA contractor report -- NASA CR-198029-198030.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Acoustic properties.; Combustion chambers.; Compressible flow.; Cross flow.; Density (Mass/volume); Euler equations of motion.; Mathematical models.; Modes (Standing waves); Shear layers.; Supersonic combustion.; Supersonic speed.; Three dimensional motion.; Vortex sheets.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0615-M (pts. 1-2).

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 2 microfiches.
Table of contents: title: pt. 1. [without special title]; title: pt. 2. 3-D modes.