TY - JOUR
T1 - Advances in CFD prediction of shock wave turbulent boundary layer interactions
AU - Knight, Doyle
AU - Yan, Hong
AU - Panaras, Argyris G.
AU - Zheltovodov, Alexander
N1 - Funding Information:
This research is supported by AFOSR under Grant No. F49620-99-1-0008 monitored by Drs. Robert Herklotz, L. Sakell, J. Schmisseur and Steve Walker, by the SCOPES 2000–2003 Program under Project No. 7SUPJ062351 and by the Russian Foundation of Basic Research under Grant No. 97-01-00885.
PY - 2003
Y1 - 2003
N2 - The paper presents a summary of recent computational fluid dynamics (CFD) simulations of shock wave turbulent boundary layer interactions. This survey was prepared as part of the activity of NATO RTO Working Group 10 which was established in December 1998, and considers results obtained subsequent to the previous survey paper on the same topic by Knight and Degrez ("Shock Wave Boundary Layer Interactions in High Mach Number Flows - A Critical Survey of Current CFD Prediction Capabilities", AGARD Advisory Report AR-319, Volume II, December 1998). Five configurations are considered: 2-D compression corner, 2-D shock impingement, 2-D expansion-compression corner, 3-D single fin and 3-D double fin. Recent direct numerical simulations (DNS), large eddy simulations (LES) and Reynolds-averaged Navier-Stokes (RANS) simulations are compared with experiment. The capabilities and limitations are described, and future research needs identified.
AB - The paper presents a summary of recent computational fluid dynamics (CFD) simulations of shock wave turbulent boundary layer interactions. This survey was prepared as part of the activity of NATO RTO Working Group 10 which was established in December 1998, and considers results obtained subsequent to the previous survey paper on the same topic by Knight and Degrez ("Shock Wave Boundary Layer Interactions in High Mach Number Flows - A Critical Survey of Current CFD Prediction Capabilities", AGARD Advisory Report AR-319, Volume II, December 1998). Five configurations are considered: 2-D compression corner, 2-D shock impingement, 2-D expansion-compression corner, 3-D single fin and 3-D double fin. Recent direct numerical simulations (DNS), large eddy simulations (LES) and Reynolds-averaged Navier-Stokes (RANS) simulations are compared with experiment. The capabilities and limitations are described, and future research needs identified.
KW - Boundary layers compressible flow
KW - Computational fluid dynamics (CFD)
KW - Direct numerical simulation (DNS)
KW - Gas dynamics
KW - Large eddy simulation (LES)
KW - Shock waves
KW - Turbulence
UR - http://www.scopus.com/inward/record.url?scp=0037328738&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0037328738&partnerID=8YFLogxK
U2 - 10.1016/S0376-0421(02)00069-6
DO - 10.1016/S0376-0421(02)00069-6
M3 - Review article
AN - SCOPUS:0037328738
SN - 0376-0421
VL - 39
SP - 121
EP - 184
JO - Progress in Aerospace Sciences
JF - Progress in Aerospace Sciences
IS - 2-3
ER -