Viscous Effects in Massively Ablating Planetary Entry Body Flowfields
- 1 July 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 11 (7) , 540-542
- https://doi.org/10.2514/3.62121
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Theoretical consideration of combustion effects on base pressure in supersonic flightSymposium (International) on Combustion, 1969
- Effect of gaseous injection on the hypersonic flow around transpiration-cooled bodies.Journal of Spacecraft and Rockets, 1969
- Diffuser Efficiency of Free-Jet Supersonic Wind Tunnels at Variable Test Chamber PressureJournal of the Aeronautical Sciences, 1952