Accession Number : AD0262099

Title :   MODELING TECHNIQUE FOR HEAT TRANSFER SIMILARITY PROBLEMS AT HIGH SPEEDS

Corporate Author : ROME UNIV (ITALY)

Personal Author(s) : BROGLIO,LUIGI ; RAVELLI,GIORGIO

Report Date : JAN 1961

Pagination or Media Count : 1

Abstract : A general method for the analysis of the heat transfer on bodies flying at very high speed is presented. In Part I, a modeling technique relative to the use of the blowdown supersonic and hypersonic wind tunnel to solve the complete similarity problems is given. In Part II, an application of the above technique is presented,AND EXPERIMENTAL RESULTS OF TURBULENT HEAT TRANSFER COEFFICIENTS ON BLUNT BODIES AT Mach Numbers 3.98 and 4.01 are presented. (Author)

Descriptors :   *AERODYNAMIC HEATING, *AIRCRAFT, *GUIDED MISSILES, *HEAT TRANSFER, BOUNDARY LAYER, HYPERSONIC CHARACTERISTICS, INSTRUMENTATION, SUPERSONIC FLOW, TEMPERATURE, TEST METHODS, WIND TUNNEL MODELS, WIND TUNNELS

Distribution Statement : APPROVED FOR PUBLIC RELEASE