Accession Number : AD0476283
Title : STAGNATION POINT HEAT TRANSFER PREDICTIONS FOR BLUNT BODIES IN HYPERVELOCITY FLOW,
Corporate Author : BOEING CO SEATTLE WA
Personal Author(s) : Ross, Peter A.
Report Date : 11 AUG 1964
Pagination or Media Count : 33
Abstract : Stagnation point heat transfer predictions from boundary layer program by E. A. Brown and A. Dusto are presented in comparison with other predictions and shock tube data. Several charts have been prepared in terms of simulation parameters, whereby, the heating rates based on these results can be quickly determined at the stagnation point of a blunt body in shock tubes, hypervelocity tunnels and gun ranges. (Author)
Descriptors : *AERODYNAMIC HEATING), (*BLUNT BODIES, HYPERSONIC CHARACTERISTICS, HYPERSONIC FLOW, STAGNATION POINT, HEAT TRANSFER, MATHEMATICAL PREDICTION, GAS IONIZATION, BOUNDARY LAYER, AIR, ARGON, ENTHALPY, COMPUTER PROGRAMMING, PRESSURE, SHOCK TUBES, HYPERSONIC WIND TUNNELS, HYPERVELOCITY GUNS, DISSOCIATION.
Subject Categories : FLUID MECHANICS
Distribution Statement : APPROVED FOR PUBLIC RELEASE