Effects of inlet air pressure, inlet air temperature, and compression ratio on maximum permissible performance obtained on single cylinder test engine with aircraft engine fuels varying from 87 octane number to 100 octane number with 1 ml of tetraethyl lead per gallon.


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    Title :

    Engine performance and knock rating of fuels for high-output aircraft engines


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1938


    Size :

    19 pages


    Remarks:

    14 Supp plates, Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Engine performance and knock rating of fuels for high-output aircraft engines

    Rothrock, A.M. / Biermann, A.E. | Engineering Index Backfile | 1938


    Knock rating of fuels

    Engineering Index Backfile | 1933


    Knock-rating of fuels

    Pye, D.R. | Engineering Index Backfile | 1933


    Knock Rating of Motor Fuels

    Barton, C. H. / Sprake, C. H. / Thornycroft, O. et al. | SAE Technical Papers | 1931


    Knock Rating of Gaseous Fuels

    Attar, A.A. | Online Contents | 2003