Accession Number : AD0750042
Title : Drag Coefficient of Cones
Descriptive Note : Final rept. 1 Mar 1970-30 Nov 1971
Corporate Author : VON KARMAN INST FOR FLUID DYNAMICS RHODE-SAINT-GENESE (BELGIUM)
Personal Author(s) : Wendt, John F.
PDF Url : AD0750042
Report Date : MAY 1972
Pagination or Media Count : 54
Abstract : The objective was to provide experimental values for cone drag coefficients in the near free molecule and transitional flow regimes including an examination of the effects of Mach number, wall speed ratio, bluntness, and specific heat ratio. A modulated force probe with a sensitivity in the microgram range was employed to measure the hypersonic drag forces on 9 degrees half-angle cones. A knowledge of the flow properties in the free jet employed for this study permitted the calculation of cone drag coefficients. The resulting values cover the flow regimes from near-free-molecular to transitional. The experimental data are presented as a function of the dimensionless parameters: wall Re number, and free-stream Knudsen number.
Descriptors : *REENTRY VEHICLES, *DRAG, *RAREFIED GAS DYNAMICS, *CONICAL BODIES, HYPERSONIC CHARACTERISTICS, KNUDSEN NUMBER, SPECIFIC HEAT, BLUNT BODIES, MODEL TESTS, FLOW FIELDS, TEST METHODS
Subject Categories : Guided Missile Reentry Vehicles
Distribution Statement : APPROVED FOR PUBLIC RELEASE