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Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data

Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data

By Sheryll Goecke Powers

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Publish Date

1978

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Office,for sale by the National Technical Information Office

Language

eng

Pages

35