Technique for measuring response of burning and propellant surface and arrangement used consisting of centrally vented cavity with propellant at one end and phase-locked mechanical driver, which excites cavity in resonant mode, at other end; bandwidth of resonance is determined by phase modulation of mechanical driver and measurement of resultant side-band amplitudes; experiments are described in which lock-on to resonance was achieved and maintained for runs of several seconds duration.


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    Titel :

    Admittance measurements of solid propellants by acoustic oscillator technique


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Foner, S.N. (Autor:in) / Hudson, R.L. (Autor:in) / Nall, B.H. (Autor:in)

    Erschienen in:

    AIAA Journal ; 2 , n 6


    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Admittance measurements of solid propellants by an acoustic oscillator technique

    FONER, S. N. / HUDSON, R. L. / NALL, B. H. | AIAA | 1964


    T-burner method of determining acoustic admittance of burning propellants

    Coates, R.L. / Horton, M.D. / Ryan, N.W. | Engineering Index Backfile | 1964


    T-burner method of determining the acoustic admittance of burning propellants

    COATES, R. L. / HORTON, M. D. / RYAN, N. W. | AIAA | 1964