论文信息 - An experimental investigation of the nozzle roughness effect on streamwise vortices in a supersonic jet - 字舞流文

An experimental investigation of the nozzle roughness effect on streamwise vortices in a supersonic jet

V. I. Zapryagaev | A. V. Solotchin

[1] Anjaneyulu Krothapalli,et al. Streamwise vortices in an underexpanded axisymmetric jet , 1991 .

[2] Philip J. Morris,et al. Measurements in subsonic and supersonic free jets using a laser velocimeter , 1979, Journal of Fluid Mechanics.

[3] H. Schlichting. Boundary Layer Theory , 1955 .

[4] J. M. Floryan,et al. Wavelength selection and growth of Goertler vortices , 1984 .

[5] M. Malik. Prediction and control of transition in supersonic and hypersonic boundary layers , 1989 .

[6] I. E. Beckwith,et al. Effects of nozzle design parameters on the extent of quiet test flow at Mach 3.5 , 1985 .

[7] E. R. V. Driest,et al. Boundary-Layer Transition at Supersonic Speeds - Three-Dimensional Roughness Effects (Spheres) , 1962 .

[8] Gregory S Elliott,et al. On streamwise vortices in high Reynolds number supersonic axisymmetric jets , 1993 .

[9] Jerzy M. Floryan,et al. On the görtler instability of boundary layers , 1991 .