General analysis of problem for fighter aircraft indicate that with design maximum level flight Mach Number of 1.5 at 35,000 ft and given military load, power plant configuration resulting in lesser gross weight, and hence cost, is basic engine without afterburning. (See also Aeronautical Eng Rev v 12 n 10 Oct 1953 p 42-47)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Afterburners -- Are they worth while?


    Additional title:

    Aeroplane


    Contributors:

    Published in:

    Aeroplane ; 85 , n 2199


    Publication date :

    1953


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Afterburners -- Are they worth while?

    Newton, F.C. | Engineering Index Backfile | 1953


    Afterburners

    Oates, Gordon C. | AIAA | 1985


    Afterburners for turbojet engines

    Cleveland, F.A. | Engineering Index Backfile | 1948


    Afterburners and Variable Nozzles

    Kress, Ralph | SAE Technical Papers | 1953


    Afterburners and variable nozzles

    Kress, R. | Engineering Index Backfile | 1952