An Experimental Study of a Hypersonic Wind-Tunnel Diffuser
- 1 February 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (2), 105-110
- https://doi.org/10.2514/8.2549
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Diffuser Efficiency of Free-Jet Supersonic Wind Tunnels at Variable Test Chamber PressureJournal of the Aeronautical Sciences, 1952
- Summary of Recent Experimental Investigations in the N.O.L. Hyperballistics Wind TunnelJournal of the Aeronautical Sciences, 1951
- High-Efficiency Supersonic DiffusersJournal of the Aeronautical Sciences, 1951
- Diffuser Investigations in a Supersonic Wind TunnelPublished by Defense Technical Information Center (DTIC) ,1951
- Supersonic Diffusers for Wind TunnelsJournal of Applied Mechanics, 1949