Accession Number : AD0749483
Title : Mass Transfer and Drag Effects on Turbulent Structure in a Hypersonic Wake.
Descriptive Note : Final rept. Jan 70-Jun 71,
Corporate Author : GENERAL ELECTRIC CO PHILADELPHIA PA RE-ENTRY AND ENVIRONMENTAL SYSTEMS DIV
Personal Author(s) : Thomas,Karl M. ; Maguire,Bernadette L.
Report Date : JUL 1971
Pagination or Media Count : 48
Abstract : A test facility/model combination has been developed and operated to obtain sufficiently high unit Reynolds numbers to achieve a range of flows which produce variations from completely laminar to fully developed turbulent body boundary layer on a 5 degree - 1/2 angle cone with a 3.85 inch diameter base. The state of the model boundary layer has been determined using thin film heat gages for a wide range of test conditions, both with and without surface blowing. Initial results have been obtained on the effect of surface flowing and the body boundary layer on the mean wake pitot profiles. (Author)
Descriptors : (*NOSE CONES, *ABLATION), (*REENTRY VEHICLES, WAKE), ATMOSPHERE ENTRY, HYPERSONIC CHARACTERISTICS, TURBULENCE, DRAG, MASS TRANSFER, FLOW FIELDS, HEAT TRANSFER, LIGHT GAS GUNS
Subject Categories : Guided Missile Reentry Vehicles
Distribution Statement : APPROVED FOR PUBLIC RELEASE