Review of publishers' experimental data relating to performance and design of diffusers for entry Mach Numbers up to 10.
Diffusers for supersonic wind tunnels
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 20 , n 9
1953
10 pages
Bibliography
Article (Journal)
English
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Investigation Of Diffusers For Two Stream Supersonic Wind Tunnels (AIAA 2016-0047)
British Library Conference Proceedings | 2016
|TIBKAT | 1952
|NTIS | 1946
|Engineering Index Backfile | 1960
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