Phenomenon associated with impingement of oblique shock waves on laminar boundary layers investigated experimentally; theoretical relations defining pressure rise to separation, to plateau, pressure resulting in incipient separation, and length of separated region are derived.
Interaction of oblique shock wave with laminar boundary layer
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 2-18-59W
1959
49 pages
Report
Englisch
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Effect of particle momentum transfer on an oblique-shock-wave/laminar-boundary-layer interaction
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