Effects of Hypersonic Inlet Flow Non-Uniformities on Stabilising Isolator Shock Systems
Author:
Affiliation:
1. Imperial College
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4716
Reference24 articles.
1. Aerodynamic Performance Analysis of a Hypersonic Inlet Isolator Using Computation and Experiment
2. Prediction of supersonic inlet unstart caused by freestream disturbances
3. Two-dimensional viscous simulation of inlet-isolator flows at Mach number 4
4. A geometrical approach for controlling pressure distributions in scramjet inlet and isolator
5. The effect of aspect ratio on isolator performance
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2. Control of Supersonic Inlet-Isolator Unstart Using Active and Passive Vortex Generators;AIAA Journal;2014-06
3. Velocimetry Measurements of Unstart of an Inlet-Isolator Model in Mach 5 Flow;AIAA Journal;2010-09
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