TY - GEN
T1 - Numerical simulation of crossing shock wave/turbulent boundary layer interaction
AU - Kong, Weixuan
AU - Zeng, Peng
AU - Yan, Chao
AU - Zhao, Rui
PY - 2012
Y1 - 2012
N2 - Numerical simulations have been captured for 3-D crossing shock wave/turbulent boundary layer interactions generated by 15-deg sharp fins mounted symmetrically on a flat plate at mach8.3. The full Reynolds-averaged Navier-Stokes equations are solved with high-resolution implicit finite-volume scheme. Turbulence closure is achieved with Spalart-Allmaras(SA), Wilcox' k-ω and Menter's Shear Stress Trans-port (SST) models. Complex crossing shock wave interactions, flowfield structures including the boundary-layer separation, centerline vortex, vortex interaction and entrainment flow have been revealed. Comparisons for profiles of the velocity vector, pressure and heat transfer distribution have been observed between calculated results and experimental measurements. Behavior of turbulence models in the complex flow have been pointed out. SST shows better performance in calculating the pressure and the velocity vector and all turbulence models over-predicted heat transfer coefficient.
AB - Numerical simulations have been captured for 3-D crossing shock wave/turbulent boundary layer interactions generated by 15-deg sharp fins mounted symmetrically on a flat plate at mach8.3. The full Reynolds-averaged Navier-Stokes equations are solved with high-resolution implicit finite-volume scheme. Turbulence closure is achieved with Spalart-Allmaras(SA), Wilcox' k-ω and Menter's Shear Stress Trans-port (SST) models. Complex crossing shock wave interactions, flowfield structures including the boundary-layer separation, centerline vortex, vortex interaction and entrainment flow have been revealed. Comparisons for profiles of the velocity vector, pressure and heat transfer distribution have been observed between calculated results and experimental measurements. Behavior of turbulence models in the complex flow have been pointed out. SST shows better performance in calculating the pressure and the velocity vector and all turbulence models over-predicted heat transfer coefficient.
KW - Hypersonic
KW - Shock/boundary-layer interaction
KW - Turbulence model
UR - http://www.scopus.com/inward/record.url?scp=84861693475&partnerID=8YFLogxK
U2 - 10.4028/www.scientific.net/AMR.516-517.954
DO - 10.4028/www.scientific.net/AMR.516-517.954
M3 - Conference contribution
AN - SCOPUS:84861693475
SN - 9783037854150
T3 - Advanced Materials Research
SP - 954
EP - 959
BT - Electrical Power and Energy Systems
T2 - 1st International Conference on Energy and Environmental Protection, ICEEP 2012
Y2 - 23 June 2012 through 24 June 2012
ER -