Quasi-three-dimensional method for determining aerothermodynamic configuration of turbine uses computer-interactive analysis and design and computer-interactive graphics. Design procedure executed rapidly so designer easily repeats it to arrive at best performance, size, structural integrity, and engine life. Sequence of events in aerothermodynamic analysis and design starts with engine-balance equations and ends with boundary-layer analysis and viscous-flow calculations. Analysis-and-design procedure interactive and iterative throughout.


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    Titel :

    Computer-Aided Design Of Turbine Blades And Vanes


    Beteiligte:
    Hsu, Wayne Q. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1988-03-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Air Cooling of Turbine Blades and Vanes

    Halls, G.A. | Emerald Group Publishing | 1967


    Cooling Modern Aero Engine Turbine Blades and Vanes

    Hare, Arthur / Malley, Harry H. | SAE Technical Papers | 1966


    Manufacture of Blades, Buckets, and Vanes For Turbine Engines

    Colwell, A. T. | SAE Technical Papers | 1955


    Boron aluminum blades and vanes

    STOLTZA, L. / GRAFF, J. | AIAA | 1981


    Impulse Mistuning of Blades and Vanes

    Hartung, Andreas | Online Contents | 2017