Investigation of Supersonic Jet Exhaust Flow by One-and Two-Equation Turbulence Models

[1]  Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air , 1991 .

[2]  J. Steger,et al.  Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods , 1981 .

[3]  Joseph G. Marvin,et al.  Turbulence modeling for computational aerodynamics , 1982 .

[4]  Navier-Stokes computations with finite-rate chemistry for LO2/LH2 rocket engine plume flow studies , 1991 .

[5]  V. C. Patel,et al.  Turbulence models for near-wall and low Reynolds number flows - A review , 1985 .

[6]  Computations of ideal and real gas high altitude plume flows , 1988 .

[7]  P. Spalart.  A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .

[8]  Meng-Sing Liou,et al.  Computational analysis of underexpanded jets in the hypersonic regime , 1991 .

[9]  Khaled S. Abdol-Hamid,et al.  A comparative study of two codes with an improved two-equation turbulence model for predicting jet plumes , 1992 .

[10]  D. M. Bushnell,et al.  Turbulence modeling in aerodynamic shear flows - Status and problems , 1991 .

[11]  Steven C. Caruso,et al.  Assessment of modeling and discretization accuracy for high-speed afterbody flows , 1991 .

[12]  T. Barth,et al.  A one-equation turbulence transport model for high Reynolds number wall-bounded flows , 1990 .

[13]  M. W. Rubesin,et al.  Assessment of compressibility corrections to the k-epsilon model in high-speed shear layers , 1992 .

[14]  D. Wilcox.  Reassessment of the scale-determining equation for advanced turbulence models , 1988 .

[15]  F. Menter.  Two-equation eddy-viscosity turbulence models for engineering applications , 1994 .

[16]  Pieter G. Buning,et al.  Numerical simulation of the Space Shuttle Launch Vehicle flowfield with real gas solid rocket plume effects , 1993 .

[17]  B. Lakshmanan,et al.  Investigation of supersonic jet plumes using an improved two-equation turbulence model , 1994 .