论文信息 - Modeling mass entrainment in a quasi-one-dimensional shock tube code - 字舞流文

Modeling mass entrainment in a quasi-one-dimensional shock tube code

A quasisteady mass-entrainment model for shock tube boundary layers, specifically for use in quasi-one-dimensional codes, is described. Using this model, we calculate shock tube test times for the turbulent regime.

Peter A. Jacobs | Con J. Doolan

[1] Bernard Grossman,et al. Characteristic-based, rotated upwind scheme for the Euler equations , 1992 .

[2] Ralph D. Watson,et al. Generalized Velocities in the Outer Region of Hypersonic Turbulent Boundary Layers , 1979 .

[3] Peter A. Jacobs. Quasi-one-dimensional modeling of a free-piston shock tunnel , 1994 .

[4] H. Mirels. Shock Tube Test Time Limitation Due to Turbulent-Wall Boundary Layer , 1964 .

[5] K. Tani,et al. Numerical study of free-piston shock tunnel performance , 1994 .

[6] Bram van Leer,et al. Progress in Multi-Dimensional Upwind Differencing , 1993 .

[7] J. J. Gottlieb,et al. Numerical investigation of high-temperature effects in the UTIAS-RPI hypersonic impulse tunnel , 1991 .

[8] Eli Turkel,et al. On Central-Difference and Upwind Schemes , 1992 .

[9] A. Jameson. Iterative solution of transonic flows over airfoils and wings, including flows at mach 1 , 1974 .

[10] Gregory J. Wilson,et al. Test times in hypersonic shock tubes , 1995 .