Abstract The technology of propulsive systems draws on a substantial body of formal fluid mechanical theory. The design of exhaust nozzles, turbine and compressor blade cascades, the analysis of the design-point operation of subsonic and supersonic inlets, etc., involve mathematically sophisticated solutions of the fluid motion and aero-thermochemical coupling between it and the medium. As difficult as some of these problems are, their basic formulation is usually reasonable clear. With enough effort, a theoretical framework can be developed and extended by controlled experimental work.


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    Title :

    Interaction Flows Due to Supersonic Secondary Jets


    Contributors:


    Publication date :

    1968-01-01


    Size :

    21 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English






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