The tests conducted on the combustion chamber model of a turbofan-ramjet combination engine are detailed. The layout of the models and the test benches on which the models were installed to conduct the tests are described. The benches are: (1) the 15,000-horsepower bench at Les Gatines on which a combustion chamber incorporating a pilot burner was defined and developed and a procedure for test data analysis was established; and (2) the K3 test bench at Saclay where the combustion chamber defined on the bench at Les Gatines was tried in simulated flight conditions at a Mach number varying from 1.5 to 4 and at altitudes reaching 100,000 ft. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental and Design Studies for Turbo-Ramjet Combination Engine Volume V - Combustion-Test Installation


    Contributors:
    P. Chaulin (author) / M. Ravel (author) / A. Gozlan (author)

    Publication date :

    1966


    Size :

    58 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Off-design Performance Analysis of Air Turbo Ramjet Engine

    Yang, I. / Lee, Y. / Yang, S. et al. | British Library Conference Proceedings | 2005


    Preliminary Design Studies of a Turbo-Ramjet Missile

    E.L. KUMM / D. BITONDO | NTIS | 1953


    An Experimental Investigation of Turbo-Ramjet Engine Intake at Mach 4

    Raju, Nandhini / Pai, Tonse Gokuldas / S B, Verma et al. | AIAA | 2020