The Transient Temperature Distribution in a Wing Flying at Supersonic Speeds
- 1 December 1950
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 17 (12), 787-807
- https://doi.org/10.2514/8.1807
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Dynamic Stability at High Speeds from Unsteady Flow TheoryJournal of the Aeronautical Sciences, 1950
- Heat Transfer to Bodies Traveling at High Speed in the Upper AtmosphereJournal of the Aeronautical Sciences, 1948