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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1959 Pratt and Whitney



    Publication date :

    1959


    Size :

    14 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English