Supersonic open cavity flow physics ascertained from algebraic turbulence model simulations-Reference-Cited by-同舟云学术

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Supersonic open cavity flow physics ascertained from algebraic turbulence model simulations

Published:1996-01-15 Issue: Volume: Page:
ISSN:
Container-title:34th Aerospace Sciences Meeting and Exhibit
language:
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Author:

Tam Chung-Jen¹,Orkwis Paul¹,Disimile Peter¹

Affiliation:

1. Cincinnati, Univ., OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-75

Reference37 articles.

1. McDearmon, R.W. "Investigation of the Flow in a Rectangular Cavity in aFlat Plateat aMachNumber of 3.55,"NASATND-523, Sept 1960.

2. Charwat, A.F., Roos, J.N.,Dewey, C.F.and Hitz, J.A. "An Investigation of Separated Flows - Part I: ThePressureField,"Journal of Aerospace Sciences, Vol.28,No.6,pp457-470. TartII:Flow Separationin the Cavity and Heat Transfer," Vol.28,No.7, pp 513-527,1961.

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1. Feedback Mechanism in Supersonic Laminar Cavity Flows;AIAA Journal;2013-01

2. Effects of Shear-Layer Characteristic on the Feedback-loop Mechanism in Supersonic Open Cavity Flows;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

3. Computations of Unsteady Separating Flows over an Oscillating Airfoil;AIAA Journal;1997-07

4. Effect of Yaw on Pressure Oscillation Frequency Within Rectangular Cavity at Mach 2;AIAA Journal;1997-07

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