Supersonic Cascade Interaction
Keyword(s):
The supersonic flow adjustment between two interacting blade rows is predicted theoretically. One of both cascades may have a constant velocity in the circumferential direction. The calculation is carried out in a quasi-stationary manner. This represents an exact solution if the constant inlet and outlet flow conditions are solely under the scope of view. Admitting the above assumptions it is possible to calculate the uniform outlet flow of the first and the associated inlet flow of the second cascade as a function of the circumferential velocity. Quantitative results are presented for flat plate cascades. However, the method is not at all restricted to these simple cases.
1978 ◽
Vol 44
(379)
◽
pp. 950-959
◽
Keyword(s):
1975 ◽
Vol 3
(2)
◽
pp. 75-82
◽
Keyword(s):
1995 ◽
Vol 36
(6)
◽
pp. 844-847
Keyword(s):
Keyword(s):