A systematic engine/airframe evaluation procedure was developed and used to assess interactions for fixed and variable geometry engine concepts in tactical aircraft. The evaluation procedure provides a rapid and inexpensive technique for evaluations of advanced engine concepts for extensive matrices of potential aircraft maneuverability and multi-mission requirements. (DePo)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Turbine engine variable cycle selection program summary


    Additional title:

    Uebersicht der Auswahlkriterien fuer Turboluftstrahltriebwerke fuer den Einbau in Militaerflugzeugen


    Contributors:
    Glaser, F.C. (author) / Weber, W.B. (author)

    Published in:

    Publication date :

    1977


    Size :

    57 Seiten


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




    Turbine Engine Variable Cycle Selection Program Summary

    F. C. Glaser / W. B. Weber | NTIS | 1977


    Variable cycle compensation in a gas turbine engine

    TERWILLIGER NEIL / BENGEA SORIN | European Patent Office | 2021

    Free access

    VARIABLE CYCLE COMPENSATION IN A GAS TURBINE ENGINE

    TERWILLIGER NEIL / BENGEA SORIN | European Patent Office | 2020

    Free access

    VARIABLE CYCLE COMPENSATION IN A GAS TURBINE ENGINE

    TERWILLIGER NEIL / BENGEA SORIN | European Patent Office | 2022

    Free access

    Variable cycle compensation in a gas turbine engine

    TERWILLIGER NEIL / BENGEA SORIN | European Patent Office | 2024

    Free access