An Experimental Documentation Of A Hypersonic Shock Wave Turbulent Boundary Layer Interaction Flow With And Without Separation

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An Experimental Documentation of a Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flow: With and Without Separation

An Experimental Documentation of a Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flow: With and Without Separation
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Total Pages : 72
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ISBN-10 : NASA:31769000530991
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Book Synopsis An Experimental Documentation of a Hypersonic Shock-wave Turbulent Boundary Layer Interaction Flow: With and Without Separation by :

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Two classes of shock-wave boundary-layer interactions were studied experimentally in a shock tunnel in which a low Reynolds number, turbulent flow at Mach 8 was