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)


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    Titel :

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


    Beteiligte:
    P. Chaulin (Autor:in) / M. Ravel (Autor:in) / A. Gozlan (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    58 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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