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
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Results of recent hypersonic and unsteady flow research at Langley Aeronautical Laboratory
Engineering Index Backfile | 1950
|