Accession Number : AD0706906
Title : LOW DENSITY HIGH TEMPERATURE GAS DYNAMICS.
Descriptive Note : Final scientific rept. 1 Nov 68-31 Oct 69,
Corporate Author : VON KARMAN INST FOR FLUID DYNAMICS RHODE-SAINT-GENESE (BELGIUM)
Personal Author(s) : Smolderen,Jean J. ; Wendt,J. F.
Report Date : 30 NOV 1969
Pagination or Media Count : 17
Abstract : Surface pressures on a flat plate with sharp leading edge were measured in a M = 1.5 monatomic gas flow. The results were in essential agreement with those recorded for a diatomic gas, but differed quantitatively from a recent theory based on a discrete ordinate solution of the BGK equation. The modulated hot-wire probe was proven conclusively to provide a measurement of local mass flux in a hypersonic flow. Surveys performed in a low density free jet showed very clearly the initial disturbance produced by the thick surrounding shock structure. The upstream influence of a sharp flat plate was measured with the modulated hot wire probe. The disturbance field was symmetrical about the leading edge and extended upstream for approximately three mean-free-paths based on a body-free stream collision. Thermographic phosphors were determined to exhibit a sensitivity of 8% change in output light intensity per deg C and to have an equivalent noise figure of 0.1C; thus they will be suitable for measuring local surface temperature at sharp leading edges. (Author)
Descriptors : (*FLAT PLATE MODELS, HYPERSONIC CHARACTERISTICS), LEADING EDGES, SHOCK WAVES, SURFACE TEMPERATURE, DENSITY, RAREFIED GAS DYNAMICS, BELGIUM
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE