Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    A control system concept for an axisymmetric supersonic inlet.


    Author / Creator :

    BURR, R. H. /BOEING CO., SUPERSONIC TRANSPORT BRANCH, SEATTLE, WASH./., CHUN, K. S.


    Contributors:
    BURR, R. H. (author)

    Published in:

    Journal of Aircraft ; 6 , 4 ; 306-311


    Publication date :

    1969-01-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Axisymmetric nose inlet effects on supersonic airloads

    FINK, M. R. / ANDERSON, W. E. | AIAA | 1983



    Performance Estimates for a Supersonic Axisymmetric Inlet System

    NORMAN E. SORENSEN AND DONALD B. SMELTZER | AIAA | 1972