Circumferential Asymmetry in Axial Flow Compressors
1966 ◽
Vol 70
(670)
◽
pp. 953-957
Keyword(s):
In this paper we are restricting our attention to those cases of circumferential inlet distortion where the distortion of the velocity profile is too large to be described as a small perturbation. Thus any theory describing the flow must use a mathematical model which is non-linear.
1995 ◽
Vol 209
(4)
◽
pp. 249-258
◽
Keyword(s):
1962 ◽
Vol 4
(2)
◽
pp. 166-176
◽
1974 ◽
Vol 13
(03)
◽
pp. 151-158
◽
Keyword(s):
Keyword(s):
1984 ◽
Vol 92
(4)
◽
pp. 529-539
◽
2000 ◽
Vol 115
(2-3)
◽
pp. 191-212
◽