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- W88539008 abstract "The results of theoretical experimental research of pressure distribution on the surface and erodynamic characteristics of burnt forms of flying vehicles which are modeled by convexo-concave shaped bodies of revolution have been presented. Experimental investigations were conducted in the supersonic wind tunnel at angles of attack from 0 to 7 degrees and with Mach number from 2 to 4. The theoretical investigation results were obtained within the framework of the inviscid perfect gas model using S.K. Godunovs relaxation method of the first order accuracy on independent variables. The complex investigation demonstrated the possibility of applying the assumed physical model of inviscid flow to define the picture of stream-lining and evaluate aerodynamic characteristics during the non-interrupted stream-lining of models under investigation." @default.
- W88539008 created "2016-06-24" @default.
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- W88539008 date "2009-01-01" @default.
- W88539008 modified "2023-09-24" @default.
- W88539008 title "Аэродинамика длинных тонких конусов с асимметричной формой затупления" @default.
- W88539008 hasPublicationYear "2009" @default.
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