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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