Instabilities of supersonic mixing layers inside a rectangular channel

Author:

TAM C.1,HU F.1

Affiliation:

1. Florida State University, Tallahassee

Publisher

American Institute of Aeronautics and Astronautics

Reference10 articles.

1. where

2. Consider the vortex sheet i n figure 3 as a rigid wall with vertical displacement y = n (x) = E sinax. On starting from the linearized equations of motion it i s easy to show that the pressure disturbances pl andp2associ

3. This work was supported by the Office of Naval Research under Grant No. NO0014-87-5-1 130. I n (A31 Ucl and Uc 2 are the mean flow velocities

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1. Effect of side confining walls on the growth rate of compressible mixing layers;Computers & Fluids;2013-11

2. Inviscid spatial stability of a compressible mixing layer. Part 3. Effect of thermodynamics;Journal of Fluid Mechanics;1991-03

3. On the turbulent mixing of compressible free shear layers;Proceedings of the Royal Society of London. Series A: Mathematical and Physical Sciences;1990-11-08

4. Numerical simulation of 3-D supersonic free shear layers;13th Aeroacoustics Conference;1990-08-17

5. Numerical simulation of a compressible shear layer;21st Fluid Dynamics, Plasma Dynamics and Lasers Conference;1990-06-18

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