Erscheint 4 Ausgaben pro Jahr
ISSN Druckformat: 1065-3090
ISSN Online: 1940-4336
Indexed in
NUMERICAL VISUALIZATION OF FLOW AROUND A SUPERSONIC FLYING VEHICLE WITH A CONICAL STABILIZER
ABSTRAKT
The paper presents numerical research of supersonic flow around the aerodynamic configuration with a conical stabilizer (flare). Analysis of flow fields and distributions of the gas-dynamic parameters was carried out. The calculated results and the experimental data are compared. A characteristic feature is revealed which is associated with the nonmonotonic character of pressure distribution on the flare.
-
Coleman, G. T. , A Study of Hypersonic Boundary Layers over a Family of Axisymmetric Bodies at Zero Incidence.
-
Glotov, G. F. , Aerothermodynamics of Flying Vehicles in Photographs.
-
Krasilshchikov, A. P. and Guryashkin, L. P. , Experimental Studies of Bodies of Revolution in Hypersonic Flows.
-
Zhilin, Yu. L and Kovalenko, V. V. , On the binding of near and far fields in the problem of sonic boom.