An experimental study of transonic shock/boundary layer interactions subject to downstream pressure perturbations-Reference-Cited by-同舟云学术

An experimental study of transonic shock/boundary layer interactions subject to downstream pressure perturbations

Published:2010-03 Issue:2 Volume:14 Page:134-142
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Bruce P.J.K.,Babinsky H.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference12 articles.

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2. Unsteady shock wave dynamics;Bruce;Journal of Fluid Mechanics,2008

3. P.J.K. Bruce, H. Babinsky, Behaviour of unsteady transonic shock/boundary layer interactions with three-dimensional effects, AIAA Paper 2009-1590, 2009

4. Experimental and numerical study of forced shock-wave oscillations in a transonic channel;Bur;Aerospace Science and Technology,2006

5. Turbulent shock–boundary layer interaction and its control;Delery;Progress in Aerospace Sciences,1985

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