Modern rockets operate at supercritical pressures with respect to the propellants. Researchers need to understand mixing and combustion beyond liquid, gas states. Shear coaxial injectors are a common choice for cryogenic liquid rocket engines. Interactions of transverse acoustics with injector's own modes and mixing need to be understood for combustion instability. Need to understand differences in response to pressure and velocity nodes. Understand what non-dimensional numbers capture the mixing of typical injectors, characterize how geometry affects mixing.


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    Titel :

    Mixing in Shear Coaxial Jets with and without Acoustics


    Beteiligte:
    I. A. Leyva (Autor:in) / S. Teshome (Autor:in) / J. Rodriguez (Autor:in) / J. Graham (Autor:in)

    Erscheinungsdatum :

    2012


    Format / Umfang :

    72 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Mixing in Shear Coaxial Jets with and without Acoustics (Briefing Charts)

    I. Leyva / S. Teshome / J. Rodriguez et al. | NTIS | 2012



    Acoustics of Under- and Over-Expanded Coaxial Jets

    Debiasi, M. / Papamoschou, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1999


    Acoustics of under- and over-expanded coaxial jets

    Debiasi, Marco / Papamoschou, Dimitri | AIAA | 1999


    Turbulent mixing of coaxial jets

    Alpinieri, L.J. | Engineering Index Backfile | 1964