Aerodynamic and Radiant Heat Input to Space Vehicles Which Re-Enter at Satellite and Escape Velocity
- 1 August 1961
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in ARS Journal
- Vol. 31 (8) , 1102-1111
- https://doi.org/10.2514/8.5726
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Stagnation Point of a Blunt Body in Hypersonic FlowJournal of the Aeronautical Sciences, 1957