TY - GEN
T1 - Physical insight into a mach 7.2 compression corner flow
AU - Ritos, Konstantinos
AU - Kokkinakis, Ioannis W.
AU - Drikakis, Dimitris
PY - 2018/1/1
Y1 - 2018/1/1
N2 - High-order implicit Large Eddy Simulations were conducted to study shock-boundary layer interaction around a 33◦ compression corner at Mach 7.2 and Reynolds number of Reθ = 3,500 based on the momentum thickness. A grid-convergence study was performed to reduce the computational uncertainty and the results were compared with experiments and theoretical predictions. Furthermore, the turbulent flow properties were analysed with respect to the Reynolds normal stress, skewness and flatness, and conclusions were drawn regarding the shock boundary layer interaction behavior.
AB - High-order implicit Large Eddy Simulations were conducted to study shock-boundary layer interaction around a 33◦ compression corner at Mach 7.2 and Reynolds number of Reθ = 3,500 based on the momentum thickness. A grid-convergence study was performed to reduce the computational uncertainty and the results were compared with experiments and theoretical predictions. Furthermore, the turbulent flow properties were analysed with respect to the Reynolds normal stress, skewness and flatness, and conclusions were drawn regarding the shock boundary layer interaction behavior.
UR - http://www.scopus.com/inward/record.url?scp=85044426989&partnerID=8YFLogxK
U2 - 10.2514/6.2018-1810
DO - 10.2514/6.2018-1810
M3 - Conference contribution
AN - SCOPUS:85044426989
SN - 9781624105241
T3 - AIAA Aerospace Sciences Meeting, 2018
BT - AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aerospace Sciences Meeting, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -