A direct method for computing the steady flow at mach number one past a given wing airfoil
1982 ◽
Vol 2
(4)
◽
pp. 389-402
◽
1962 ◽
Vol 84
(6)
◽
pp. 1063-1064
◽
Keyword(s):
1978 ◽
Vol 60
(4)
◽
pp. 591-594
◽