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The behavior of a compressible turbulent boundary layer in a shock-wave-induced adverse pressure gradient
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Authors:
Rose, William C.
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United States.
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Ames Research Center.
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University of Washington.
Year: 1973 Publisher: Washington, D.C. : National Aeronautics and Space Administration,
Year: 1973 Publisher: Washington, D.C. : National Aeronautics and Space Administration,
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Abstract
Keywords
Shock waves. --- Turbulent boundary layer. --- Shock waves. --- Pressure gradients. --- Turbulent boundary layer.
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