Wind-Tunnel Tests for Temperature Recovery Factors at Supersonic Velocities
- 1 February 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (2) , 97-100
- https://doi.org/10.2514/8.1866
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- SUPERSONIC FLOW PAST SLENDER POINTED BODIESThe Quarterly Journal of Mechanics and Applied Mathematics, 1949