TY - GEN
T1 - High performance parallel implicit computations of three-Dimensional supersonic magnetohydrodynamics using PETSc library
AU - Wan, Tian
AU - Candler, Graham V.
PY - 2007
Y1 - 2007
N2 - A three-dimensional MHD solver is described in the paper. The solver simulates reacting flows with nonequilibrium between translational-rotational, vibrational and electron translational modes. Also included are models for electrical conductivity, electron thermal conductivity and collision frequencies. The conservation equations are discretized with implicit time marching and the second-order Steger-Warming scheme, and the resulted linear system is solved iteratively with a fully coupled parallel preconditioned GMRES method that is implemented by the PETSc package. The results of convergence tests are plotted, which show good scalability and convergence acceleration between two and Ave times when compared with the DPLR method. Then Ave test runs are conducted simulating the experiments done at the NASA Ames MHD channel, and the calculated pressures, temperatures, electrical conductivity, back EMF and now accelerations are shown to agree with the experimental data. A scramjet-driven Diagonal Conducting Wall MHD generator is also simulated which works at the design parameters of the HVEPS program taken from the reference paper. The scramjet model is taken from University of Queensland, and one set of their scramjet experiments is simulated with both fuel on and off. Then MHD power generation computation is performed on top of the scramjet model, and plotted are conductivity and Hall parameter distribution. The computed power generation is 2.2MW which is within the design power regime.
AB - A three-dimensional MHD solver is described in the paper. The solver simulates reacting flows with nonequilibrium between translational-rotational, vibrational and electron translational modes. Also included are models for electrical conductivity, electron thermal conductivity and collision frequencies. The conservation equations are discretized with implicit time marching and the second-order Steger-Warming scheme, and the resulted linear system is solved iteratively with a fully coupled parallel preconditioned GMRES method that is implemented by the PETSc package. The results of convergence tests are plotted, which show good scalability and convergence acceleration between two and Ave times when compared with the DPLR method. Then Ave test runs are conducted simulating the experiments done at the NASA Ames MHD channel, and the calculated pressures, temperatures, electrical conductivity, back EMF and now accelerations are shown to agree with the experimental data. A scramjet-driven Diagonal Conducting Wall MHD generator is also simulated which works at the design parameters of the HVEPS program taken from the reference paper. The scramjet model is taken from University of Queensland, and one set of their scramjet experiments is simulated with both fuel on and off. Then MHD power generation computation is performed on top of the scramjet model, and plotted are conductivity and Hall parameter distribution. The computed power generation is 2.2MW which is within the design power regime.
UR - http://www.scopus.com/inward/record.url?scp=35649026854&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=35649026854&partnerID=8YFLogxK
U2 - 10.2514/6.2007-4367
DO - 10.2514/6.2007-4367
M3 - Conference contribution
AN - SCOPUS:35649026854
SN - 1563479001
SN - 9781563479007
T3 - Collection of Technical Papers - 38th AIAA Plasmadynamics and Lasers Conference
SP - 658
EP - 674
BT - Collection of Technical Papers - 38th AIAA Plasmadynamics and Lasers Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 38th AIAA Plasmadynamics and Lasers Conference
Y2 - 25 June 2007 through 28 June 2007
ER -