Investigation Of Supersonic Turbulent Boundary Layer Separation On A Compression Ramp By An Integral Method

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Investigation of Supersonic Turbulent Boundary-layer Separation on a Compression Ramp by an Integral Method

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Total Pages	: 66
Release	: 1977
ISBN-10	: NASA:31769000539885
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Rating	: 4/5 ( Downloads)

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Basic research programs are reported with fundamental applications to supersonic flight. The experimental studies made use of the unique capabilities of the hig

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An Experimental Investigation of the Supersonic Turbulent Boundary Layer in a Moderate Adverse Pressure Gradient. Part II. Analysis of the Experimental Data

Authors: W. B. Sturek

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Type: BOOK - Published: 1971 - Publisher:

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The experimental data reported in Part 1 are analyzed. Turbulent boundary layer equations applicable to compressible flow over a surface with longitudinal curva