A parametric cycle analysis and a preliminary recuperator design study were conducted for a 500-hp intermediate rated power (IRP) recuperative helicopter engine. The U-tube recuperator with airflow inside the tubes and single cross flow gas path was found to be the lightest design in the 0.6-0.8 effectiveness range considered for the cycle analysis. (Stoehr)


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    Titel :

    Regenerative engine analysis program


    Weitere Titelangaben:

    Analyse eines rekuperativen Hubschrauberantriebs


    Beteiligte:
    Schwaar, P. (Autor:in) / Dale, J. (Autor:in) / Banks, J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1981


    Format / Umfang :

    199 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch





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