Design of Nozzles for Individual Cylinder Exhaust Jet Propulsion System. (Originally issued as Advance Confidential Report Apr 1941)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Design of nozzles for individual cylinder exhaust jet propulsion system


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:
    Pinkel, B. (author) / Turner, L.R. (author) / Voss, F. (author)


    Publication date :

    1941


    Size :

    34 pages


    Remarks:

    Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



    Design of nozzles for the individual cylinder exhaust jet propulsion system

    Pinkel, Benjamin / Turner, L. Richard / Boss, Fred | TIBKAT | 1941


    Tests of exhaust propulsion nozzles

    Campbell, Paul J | NTRS | 1943


    Tests of exhaust propulsion nozzles

    Campbell, Paul J. | TIBKAT | 1943


    Optimized supersonic exhaust nozzles for hypersonic propulsion

    NICKERSON, G. / DUNN, S. / MIGDAL, D. | AIAA | 1988