Calculation of multistage turbomachinery using steady characteristic boundary conditions
36th AIAA Aerospace Sciences Meeting and Exhibit ; 1998 ; Reno , NV , U.S.A.
01.01.1998
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Calculation of Multistage Turbomachinery Using Steady Characteristic Boundary Conditions
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