Power and heat stress conditions of geometrically similar engines are discussed; advantages accruing from smaller cylinder dimensions are higher specific horsepower, lower weight per horsepower, lower piston temperature, and less frontal area, with reduced detonation tendency. English translation of paper indexed in Engineering Index 1939 p 617, from Jahrbuch 1938 der Deutsche Luftfahrtforschung.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Heat transfer in geometrically similar cylinders


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Beteiligte:
    Riekert, P. (Autor:in) / Held, A. (Autor:in)


    Erscheinungsdatum :

    1941


    Format / Umfang :

    10 pages


    Anmerkungen:

    1 Supp plate


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




    Heat transfer in geometrically similar cylinders

    Riekert, P / Held, A | NTRS | 1941


    Geometrically similar models

    Ridgely-Nevitt, Cedric | IOS Press | 1959


    Comparing the performance of geometrically similar airplanes

    Munk, Max M / Warner, Edward P | NTRS | 1924



    Tests on three geometrically-similar ship models

    Saunders, H.E. | Engineering Index Backfile | 1933