In studying an ideal cycle relevant to aircraft propulsion, one can have a good insight into the relevant important parameters that give the performance parameters of a given system. For such a study, the following assumptions are usually taken:


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    Title :

    Thermodynamic Ideal Cycle Analysis


    Additional title:

    Springer Aerospace Techn.


    Contributors:
    Bose, Tarit (author)


    Publication date :

    2012-05-15


    Size :

    60 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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