Abstract Fundamental aerothermodynamic equations derived in Chapter 1 may now be applied for aerodynamic design of axial flow compressors and turbines. A typical sketch of an axial flow compressor is shown in Fig. 3-1.


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    Title :

    Aerodynamic Design of Axial Flow Compressors and Turbines


    Contributors:


    Publication date :

    1968-01-01


    Size :

    29 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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