Experimental Lift and Drag of a Series of Glide Configurations at Mach Numbers 12.6 and 17.5
- 1 April 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (4) , 410-419
- https://doi.org/10.2514/8.9475
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- HYPERSONIC FLOW-BLAST ANALOGYPublished by Defense Technical Information Center (DTIC) ,1961