The calculation of the steady-state quasi-three-dimensional flow of a nonviscous nonheat-conducting gas in the nozzles and moving blade rows of axial turbomachines having arbitrary flow section and blade geometry is considered. The system of equations for quasi-three-dimensional flow is given together with the boundary conditions. A buildup method is used to calculate the flow in conjunction with a Godunov finite-difference scheme. This makes it possible to investigate flows at subsonic, transonic, and supersonic velocities.
Quasi-three-dimensional flow of gas in turbomachine blade row
Quasidreidimensionale Gasstroemung zwischen den Schaufeln eines Turboverdichters
Power Engineering, New York ; 22 , 3 ; 137-143
1984
7 Seiten, 12 Quellen
Aufsatz (Zeitschrift)
Englisch
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