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.


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    Title :

    Quasi-three-dimensional flow of gas in turbomachine blade row


    Additional title:

    Quasidreidimensionale Gasstroemung zwischen den Schaufeln eines Turboverdichters


    Contributors:

    Published in:

    Publication date :

    1984


    Size :

    7 Seiten, 12 Quellen


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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