Performance of annular combustor of turbojet engine was investigated in combustion laboratory to determine whether correlation exists between performance of combustor and altitude operational limits of engine revealed by altitude wind tunnel research. (See also - (discussion) p 278, 344; Nat Advisory Committee Aeronautics -- Tech Note n 1357 July 1947 26 p, 26 supp plates;)


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    Title :

    Effect of combustor-inlet conditions on performance of annular turbojet combustor


    Additional title:

    Soc Automotive Engrs -- Trans


    Contributors:


    Publication date :

    1947


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Effect of combustor-inlet conditions on performance of Annular Turbojet Combustor

    Childs, J.H. / McCafferty, R.J. / Surine, C.W. | Engineering Index Backfile | 1947


    Effect of combustor-inlet conditions on performance of annular turbojet combustor

    Childs, J.H. / McCafferty, R.J. / Surine, O.W. | Engineering Index Backfile | 1947


    Effect of COMBUSTOR-INLET CONDITIONS on Combustion in Turbojet Engines

    CHILDS, J. HOWARD / SURINE, OAKLEY W. / McCAFFERTY, RICHARD J. | SAE Technical Papers | 1947


    Performance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions

    Butze, Helmut F. / Trout, Arthur M. / Moyer, Harry M. | TIBKAT | 1969


    Investigation of Combustion Performance of Turbojet Combustor

    K. Homma / S. Horiuchi / T. Otsuka | NTIS | 1970