Behaviour of unsteady transonic shock/boundary layer interactions with three-dimensional effects
Author:
Affiliation:
1. University of Cambridge
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1590
Reference12 articles.
1. Forced oscillation experiments in supercritical diffuser flows
2. Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle
3. Mechanism of Shock Wave Oscillation in Transonic Diffusers
4. Experimental and numerical study of forced shock-wave oscillations in a transonic channel
5. Unsteady shock wave dynamics
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1. Numerical study of oblique shock-wave/boundary-layer interaction considering sidewall effects;Journal of Fluid Mechanics;2015-02-20
2. Experimental Study on Pressure Fluctuations in the Shock/boundary Layer Interaction of an Axisymmetric Body;Applied Mechanics and Materials;2011-07
3. Direct numerical simulation of transonic shock/boundary layer interaction under conditions of incipient separation;Journal of Fluid Mechanics;2010-06-24
4. An experimental study of transonic shock/boundary layer interactions subject to downstream pressure perturbations;Aerospace Science and Technology;2010-03
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