Comprehensive mesh study for a Direct Numerical Simulation of the transonic flow at Rec = 500,000 around a NACA 0012 airfoil
2005 ◽
Vol 34
(9)
◽
pp. 1096-1114
◽
2003 ◽
Vol 71
(1-4)
◽
pp. 203-220
◽
2001 ◽
Vol 11
(PR6)
◽
pp. Pr6-331-Pr6-338
◽