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 Soc Automotive Engrs -- Trans v 1 n 2 Apr 1947 p 266-78 (discussion) 278, 344)


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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    26 pages


    Remarks:

    26 Supp Plates


    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 an Annular Turbojet Combustor

    J. H. Childs / R. J. McCaffferty / O. W. Surine | NTIS | 1947


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

    Childs, J. Howard / McCafferty, Richard J. / Surine, Oakley W. | TIBKAT | 1947


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

    Childs, J Howard / Mccafferty, Richard J / Surine, Oakley W | NTRS | 1947


    Effect of combustor-inlet condition on performance of an annular turbojet combustor

    Childs, Howard J / Mccafferty, Richard J / Surine, Oakley W | NTRS | 1947