Experimental Study on Thermal Protection System by Opposing Jet in Supersonic Flow
Authors:
- 1 January 2006
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 43 (1) , 233-235
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Thermal protection and drag reduction with use of spike in hypersonic flow2001
- The flow of a jet from a body opposing a supersonic free streamJournal of Fluid Mechanics, 1966
- An experimental investigation of the effect of ejecting a coolant gas at the nose of a bluff bodyJournal of Fluid Mechanics, 1960