Rocket propelled research model was flown in tests at Langley Research Station; local Reynolds numbers based on body length to measurement station varied from 2×106 to 138× 106; local Stanton numbers obtained for each section of body are compared with theoretical values; recovery factors, transition Reynolds numbers, and some heat transfer data at angle of attack.
Measurements of aerodynamic heat transfer on 15° cone-cylinder-flare configuration in free flight at Mach numbers up to 4.7
NASA -- Tech Note
1961
61 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.