Experimental and numerical study of forced shock-wave oscillations in a transonic channel

Author:

Bur R.,Benay R.,Galli A.,Berthouze P.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. Modeling of controlled shock-wave/boundary-layer interactions in transonic channel flow;Benay;AIAA J.,2001

2. Investigation of an asymmetrical shock-wave/boundary-layer interaction in a supersonic planar nozzle;Benay;Canadian Aeronautics and Space (CAS) J.,2005

3. Applications of a Navier–Stokes solver to calculations of missile or aircraft afterbody flows;Benay;Aerospace Res.,1995

4. Two-equation k–σ turbulence model: application to a supersonic base flow;Benay;AIAA J.,2001

5. P. Berthouze, Experimental and theoretical study of an unsteady transonic channel flow, Ph.D. Thesis, University of Poitiers, France, 2003

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