Accession Number : AD0607970
Title : INVESTIGATION OF A HYPERSONIC FLOW OF SLIGHTLY RAREFIED VISCOUS GAS AROUND A FLAT PLATE,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Galkin,V. S.
Report Date : 24 JUL 1963
Pagination or Media Count : 11
Abstract : Calculation of drag coefficient of a flat semi-infinite heat-insulated plate in a hypersonic gas flow with slip is described. It is assumed that the region of flow between joined strong jumps of the packing and the plate consists of a non-viscous zone and laminar boundary layer. The strong interaction of the jump with the layer is considered. In calculation of the boundary layer the integral form of equation of pulses with linear profile of speed is used and taking into account the speed of slip. Parameters of flow on the external boundary of the boundary layer are calculated by the method of tangential wedges.
Descriptors : (*FLAT PLATE MODELS, HYPERSONIC FLOW), (*DRAG, FLAT PLATE MODELS), BOUNDARY LAYER, LAMINAR BOUNDARY LAYER, GAS FLOW, THERMAL INSULATION, VISCOSITY, USSR
Distribution Statement : APPROVED FOR PUBLIC RELEASE