Heat-transfer Measurements on Two Bodies of Revolution at a Mach Number of 3.12
Auteur : John R. Jack, N. S. Diaconis
Date de publication : 1956
Éditeur : National Advisory Committee for Aeronautics
Nombre de pages : 36
Résumé du livre
The laminar-heat-transfer coefficients obtained from the conical portion of the cone cylinder agree closely with theory at all temperature levels when corrected for the axial temperature distribution. Experimentally and analytically, there seems to be no significant effect of temperature level on the heat-transfer coefficient. The laminar data obtained from the parabolic-cylinder model agree closely with theory when the axial pressure distribution is considered and the data are corrected for the axial temperature distribution.