Background and development program; list of current applications for engine; selection of airflow capacity at approximately 50 lb/sec; factors considered in choice of 9-stage compressor to maintain max relative Mach number at 1.0 and average stage pressure ratio at 1. 24; use of IBM calculation in compressor design procedure; comparison of JT12 with JT4 relating to various design features.


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    Titel :

    JT12 Pratt and Whitney aircraft's 3000 Lb. Thrust turbojet engine


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Phinney, D.G. (Autor:in)

    Kongress:

    SAE Meeting ; 1959 Pratt and Whitney



    Erscheinungsdatum :

    1959


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    THE JT12 PRATT & WHITNEY AIRCRAFT'S 3000 LB. THRUST TURBOJET ENGINE

    PHINNEY, DAVIS G. | SAE Technical Papers | 1959




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