Engine test results for simulated altitude conditions using displacer piston combustion chamber on 5-in. by 7-in. single cylinder engine operating at 2000 rpm; analysis of results for which inlet air temperature and pressure were varied independently indicates that maximum engine performance cannot be corrected reliably on inlet air density or weight of air charge basis.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Compression-ignition engine performance at altitude


    Additional title:

    Soc Automotive Engrs -- J


    Contributors:


    Publication date :

    1937


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Compression-Ignition Engine Performance at Altitude

    Moore, Charles S. / Collins, John H. | SAE Technical Papers | 1937


    Prechamber compression-ignition engine performance

    Moore, C.S. / Collins, Jr., J.H. | Engineering Index Backfile | 1937


    Prechamber compression-ignition engine performance

    Moore, C.S. / Collins, Jr., J.H. | Engineering Index Backfile | 1937


    Prechamber compression-ignition engine performance

    Moore, C.S. / Collins, Jr., J.H. | Engineering Index Backfile | 1937


    Prechamber compression-ignition engine performance

    Moore, Charles S. / Collins, John H. | TIBKAT | 1936