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Heat Transfer for Mach Numbers Up to 2.2 and Pressure Distributions for Mach Numbers Up to 4.7 From Flight Investigations of a Flat-Face-Cone and a Hemisphere-Cone
Author:
Speegle, Katherine C.
Additional Authors:
Chauvin, Leo T.
Year:
1958
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L58B18
Link:
https://digital.library.unt.edu/ark:/67531/metadc63975/
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