Large-scale streamwise vortices in the supersonic part of a permeable nozzle

被引：5

作者：

Zaikovskii V.N. ^{[1
]}

Kiselev S.P. ^{[1
]}

Kiselev V.P. ^{[1
]}

机构：

[1] Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences

来源：

Journal of Applied Mechanics and Technical Physics | 2005年 / 46卷 / 5期

关键词：

Gas inflow and outflow; Large-scale streamwise vortices; Nozzle; Porous wall; Supersonic flow;

D O I：

10.1007/s10808-005-0122-5

中图分类号：

学科分类号：

摘要：

Large-scale streamwise vortices in the vicinity of a perforated wall in the supersonic part of the nozzle are studied. The governing effect of gas inflow through a perforated wall on origination and parameters of streamwise vortices is experimentally established. © Springer Science+Business Media, Inc. 2005.

引用

页码：670 / 676

页数：6

共 8 条

[1]

Grozdovskii G.L., Nikol'skii A.A., Svishchev G.P., Taganov G.I., Supersonic Gas Flows in Perforated Boundaries, (1967)

[2]

Zaikovskii V.N., Kiselev V.P., Kiselev S.P., Et al., Effect of a porous insert in the supersonic part of the nozzle in changes in the nozzle thrust, Dokl. Ross. Akad. Nauk, 401, 4, pp. 479-482, (2005)

[3]

Zapryagaev V.I., Solotchin A.V., Spatial flow structure at the initial part of a supersonic underexpanded jet, (1988)

[4]

Zheltovodov A.A., Shulein E.H., Yakovlev V.N., Development of a turbulent boundary layer under conditions of mixed interaction with shock waves and expansion waves, (1983)

[5]

Zaikovskii V.N., Melamed B.M., Vortex flows in SRM nozzles, Stability of Homogeneous and Heterogeneous Fluid Flows, pp. 183-186, (2000)

[6]

Melamed B.M., Zaikovskii V.N., An experimental study of vortex structures in gas dynamic duct with swiveling nozzle, Proc. of the IX Int. Conf. on the Method Aerophysical Research, pp. 189-192, (1998)

[7]

Loitsyanskii L.G., Mechanics of Liquids and Gases, (1966)

[8]

Landau L.D., Lifshits E.M., Course of Theoretical Physics, Vol. 6: Fluid Mechanics, (1987)

← 1 →