Theoretical Drag Prediction for Trailing Decelerators at Supersonic Speeds
- 1 December 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (12) , 1022-1028
- https://doi.org/10.2514/3.59200
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Inviscid hypersonic flow past smooth symmetric bodiesAIAA Journal, 1964
- Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause SeparationJournal of the Aeronautical Sciences, 1953