Effects of surface temperature and Reynolds number on heat transfer to the Shuttle Orbiter leeward fuselage
- 26 January 1976
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Lee surface flow phenomena over Space Shuttle at large angles of attack at M infinity = 6Published by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Effect of Nose Geometry on the Aerothermodynamic Environment of Shuttle Entry ConfigurationsJournal of Spacecraft and Rockets, 1974
- Lee-surface vortex effects over configurations in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Transformations for infinite regions and their application to flow problems.AIAA Journal, 1969