Shock interference heat transfer to tank configurations mated to a straight-wing space shuttle orbiter at mach number 10.3/

Main Author: Crawford, Davis H.
Corporate Authors: United States National Aeronautics and Space Administration, United States. National Aeronautics and Space Administration, Langley Research Center
Format: Book
Language:English
Published: Washington, D.C.: National Aeronautics and Space Administration , 1976
Series:NASA technical note NASA TN D-8203
Subjects:

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