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. (see also abstract in Aviation Week v 53 n 5 July 1950 p 22, 24)
Results of recent hypersonic and unsteady flow research at Langley Aeronautical Laboratory
J Applied Physics
Journal of Applied Physics ; 21 , n 7
1950
10 pages
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
|