Accession Number : AD0262627

Title :   AN EXPERIMENTAL TECHNIQUE TO MEASURE HEAT TRANSFER FLUXES AT HIGH SPEEDS: TURBULENT HEAT TRANSFER DATA ON A BLUNT BODY AT M 3.98

Corporate Author : ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s) : BROGLIO, L. ; BUONGIORNO, C.

Report Date : APR 1960

Pagination or Media Count : 12

Abstract : A technique is presented for measuring heat transfer rates on a model and for fixing the temperature distribution at a given value. The technique is applied to the particular case of turbulent heat transfer on a blunt body at a Mach number of 3.98. (Author)

Descriptors :   *AERODYNAMIC CHARACTERISTICS, *BLUNT BODIES, *BODIES OF REVOLUTION, *HEAT TRANSFER, *SUPERSONIC FLOW, AERODYNAMIC CONFIGURATIONS, INSTRUMENTATION, MEASUREMENT, SUPERSONIC WIND TUNNELS, TEST METHODS, TURBULENCE, WIND TUNNEL MODELS.

Distribution Statement : APPROVED FOR PUBLIC RELEASE