On the instability of inviscid, compressible free shear layers
Creators
Abstract
The linear spatial instability of inviscid compressible laminar mixing of two parallel streams, comprised of the same gas, has been investigated with respect to two-dimensional wave disturbances. The effects of the velocity ratio, temperature ratio, and the temperature profile across the shear layer have been examined. A nearly universal dependence of the normalized maximum amplification rate on the convective Mach number is found, with the normalized maximum amplification rate decreasing significantly with increasing convective Mach number in the subsonic region. These results are in accord with those of recent growth rate experiments in compressible turbulent free shear layers and other similar recent calculations.
Additional Information
Copyright © 1988 by Mei Zhuang. Published by the American Institute of Aeronautics and Astronautics, Inc. with permission. AIAA-88-3538-CP. We would like to thank Dr. Dimitri Papamoschou, Mr. Paul Miller and Mr. Cliff Frieler for their helpful discussions and assistance. This work was supported by the Air Force Office of Scientific Research Grants No. 83-0213 and 88-0155.Attached Files
Published - on_the_instability_of_inviscid.pdf
Files
on_the_instability_of_inviscid.pdf
Additional details
Identifiers
- Eprint ID
- 50584
- Resolver ID
- CaltechAUTHORS:20141020-155658655
Funding
- Air Force Office of Scientific Research (AFOSR)
- 83-0213
- Air Force Office of Scientific Research (AFOSR)
- 88-0155
Dates
- Created
-
2014-10-21Created from EPrint's datestamp field
- Updated
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2021-11-10Created from EPrint's last_modified field
Caltech Custom Metadata
- Caltech groups
- GALCIT