论文信息 - A Design of Experiments Study for the HIFiRE Flight 2 Ground Test Computational Fluid Dynamics Results - 字舞流文

A Design of Experiments Study for the HIFiRE Flight 2 Ground Test Computational Fluid Dynamics Results

Michael Bynum | Robert Baurle

[1] Todd Barhorst,et al. The HIFiRE Flight 2 Experiment: An Overview and Status Update , 2009 .

[2] J. Edwards. A low-diffusion flux-splitting scheme for Navier-Stokes calculations , 1997 .

[3] Jiwen Liu,et al. Combustor Operability and Performance Verification for HIFiRE Flight 2 , 2011 .

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

[5] Mark J. Anderson,et al. RSM Simplified: Optimizing Processes Using Response Surface Methods for Design of Experiments, Second Edition , 2004 .

[6] Richard L. Gaffney. Design of Mach-4 and Mach-6 Nozzles for the NASA LaRC 8-Ft High Temperature Tunnel , 2009 .

[7] R W Guy,et al. The NASA Langley Scramjet Test Complex , 1996 .

[8] Neal E. Hass,et al. HIFiRE Direct-Connect Rig (HDCR) Phase I Scramjet Test Results from the NASA Langley Arc-Heated Scramjet Test Facility , 2011 .

[9] David Wilcox. Wall matching, a rational alternative to wall functions , 1989 .

[10] B. Hjertager,et al. On mathematical modeling of turbulent combustion with special emphasis on soot formation and combustion , 1977 .