Published 2015
| metadata_only
Book Section - Chapter
Geometric Acoustics in High-Speed Boundary Layers
- Creators
- Parziale, N. J.
- Shepherd, J. E.
- Hornung, H. G.
- Others:
- Bonazza, R.
- Ranjan, D.
Abstract
A key mechanism responsible for the instability of high-speed boundary layers are the high-frequency modes discovered by Mack [1]. These modes are primarily acoustic in nature, are always present if the edge Mach number is sufficiently large, and are the dominant instability mechanism when the wall temperature is sufficiently low compared to the recovery temperature.
Additional Information
© 2015 Springer International Publishing Switzerland.
Additional details
- Eprint ID
- 78410
- DOI
- 10.1007/978-3-319-16835-7_114
- Resolver ID
- CaltechAUTHORS:20170621-105808727
- Created
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2017-06-21Created from EPrint's datestamp field
- Updated
-
2021-11-15Created from EPrint's last_modified field
- Caltech groups
- GALCIT