DTIC ADA258861: An Experimental Study of the Driving Mechanism and Control of the Unsteady Shock Induced Turbulent Separation in a Mach 5 Compression Corner Flow.

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Author:Defense Technical Information Center
Language:English
File size:7.1 MB
Number of page:278
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Similar DTIC ADA258861: An Experimental Study of the Driving Mechanism and Control of the Unsteady Shock Induced Turbulent Separation in a Mach 5 Compression Corner Flow.

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