Limitations of specifications for turbine engine fuels are given many of which relate to engine characteristics; limitations of interest to airframe designer; desirable specification for fuel that will give greatest overall profit for airlines; until such fuel is available, JP4 appears satisfactory compromise.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    What fuel characteristics mean to turbine engine airplane


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:
    Weise, C.A. (author)

    Conference:

    Society of Automotive Engineers -- Meeting (Southern California Section) ; 1957 Fuels



    Publication date :

    1957


    Size :

    8 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    WHAT FUEL CHARACTERISTICS MEAN TO THE TURBINE ENGINE AIRPLANE

    WEISE, C. A. | SAE Technical Papers | 1957


    Saurer fuel injection airplane engine

    Ostertag, A. | Engineering Index Backfile | 1948


    Turbine engine propelled airplane having an acoustic baffle

    JODET NORMAN BRUNO ANDRE / GONZALEZ JEREMY PAUL FRANCISCO / ROLLAND HERVE | European Patent Office | 2021

    Free access

    A TURBINE ENGINE PROPELLED AIRPLANE HAVING AN ACOUSTIC BAFFLE

    JODET NORMAN BRUNO ANDRE / GONZALEZ JEREMY PAUL FRANCISCO / ROLLAND HERVE | European Patent Office | 2018

    Free access

    Gas-Turbine Engine Control System of the Unmanned Airplane

    Kulik, A. S. / Symonov, V. F. / Pasichnik, S. N. et al. | British Library Conference Proceedings | 2004