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Free-Flight Aerodynamic-Heating Data to a Mach Number of 15.5 on a Blunted Conical Nose With a Total Angle of 29 Degrees
Author:
Bland, William M., Jr.
Additional Authors:
Rumsey, Charles B., Lee, Dorothy B.
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L57F28
Link:
https://digital.library.unt.edu/ark:/67531/metadc63793/
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