Experimental investigation of gamma effects on heat transfer to a 0.006 scale Shuttle Orbiter at Mach 6

This publication has 3 references indexed in Scilit:

• Approximate method of predicting heating on the windward side of Space Shuttle Orbiter and comparisons with flight data
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1982
• A DATA REDUCTION PROGRAM FOR HOTSHOT TUNNELS BASED ON THE FAY-RIDDELL HEAT-TRANSFER RATE USING NITROGEN AT STAGNATION TEMPERATURES FROM 1500 TO 5000 K
  Published by Defense Technical Information Center (DTIC) ,1964
• Theory of Stagnation Point Heat Transfer in Dissociated Air
  Journal of the Aerospace Sciences, 1958