Review of current studies of compressible flow problems connected with extremely high speeds and altitudes contemplated in supersonic aircraft design; design features of 11-in. hypersonic tunnel; air condensation experiments; flow visualization at low pressures; boundary layer effects at hypersonic speeds; research on unsteady flows. (Abstract) (See also J Applied Physics v 21 n 7 July 1950 p 619-28)
Results of recent hypersonic and unsteady flow research at Langley Aeronautical Laboratory
Aviation Week
Aviation Week ; 53 , n 5
1950
Aufsatz (Zeitschrift)
Englisch
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Results of recent hypersonic and unsteady flow research at Langley Aeronautical Laboratory
Engineering Index Backfile | 1950
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