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 Page: 1 of 61
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" --_.- _ RM L
R E S A RH - A M E M OA N D U
RES-AR-H MEO A ....
R ES EARCH M EMORAN DU M
HEAT TRANSFER FOR MACH NUMBERS UP
TO 2.2 AND PRESSURE DISTRIBUTIONS FOR MACHW
TO 4.7 FROM FLIGHT INVESTIGATIONS OF A FLAT-
AND A HEMISPHERE-CONE
By Katherine C. Speegle, Leo T. Chauvin,
and Jack C. Heberlig
Langley Aeronautical Laboratory
Langley Field, Va.
NATIONAL ADVISORY COMMITTEE
May 8, 1958
S AFMDC DAS '58-33 319
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Speegle, Katherine C.; Chauvin, Leo T. & Heberlig, Jack C. 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, report, May 8, 1958; (digital.library.unt.edu/ark:/67531/metadc63975/m1/1/: accessed January 15, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.