A Similarity Law for the Normal Force on a Delta Wing at Hypersonic Speeds
- 1 February 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 26 (2) , 119-120
- https://doi.org/10.2514/8.7956
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949