Research of a shock wave interaction with a 'thick' boundary layer at Mach numbers M = 3-4
2016 ◽
Vol 23
(2)
◽
pp. 173-183
◽
Keyword(s):
1958 ◽
Vol 9
(5-6)
◽
pp. 312-331
◽
Keyword(s):
1960 ◽
Vol 27
(5)
◽
pp. 348-356
◽
Keyword(s):
Keyword(s):
Numerical investigations of shock wave interaction with laminar boundary layer on compressor profile
2016 ◽
Vol 760
◽
pp. 012023
◽
Keyword(s):
2017 ◽
Vol 43
(6)
◽
pp. 570-573
◽
Keyword(s):
1985 ◽
pp. 103-111
Keyword(s):
Keyword(s):