A flow-separation spike for hypersonic control of a hemisphere-cylinder
- 1 January 1964
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (1) , 159-161
- https://doi.org/10.2514/3.2255
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Flow inclination measurements in hypersonic tunnelsAIAA Journal, 1964
- AIR CONDENSATION IN A HYPERSONIC WIND TUNNELAIAA Journal, 1963