This project is intended to characterize the transient spray from a high pressure swirl injector. The spray regions were identified as the leading edge, cone, trailing edge, and vortex cloud. Each region was influenced somewhat differently by changes in the operational parameters. Increasing the ambient chamber pressure increased the droplet size in all regions of the spray. Increasing the fluid pressure reduced the droplet size in all regions of the spray, except for the vortex cloud. Increasing the swirl of the fluid leaving the fuel injector increased the size of the droplets in the leading edge and cone region.


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    Titel :

    Characterization of the Transient Spray from a High Pressure Swirl Injector


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    International Congress & Exposition ; 1994



    Erscheinungsdatum :

    1994-03-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Characterization of a transient spray from a high pressure swirl injector

    Evers,L.W. / Michigan Technological Univ.,US | Kraftfahrwesen | 1994


    Transient Spray Cone Angles in Pressure-Swirl Injector Sprays

    Assanis, Dennis N. / Snyder, Jordan A. / Grover, Ronald O. et al. | SAE Technical Papers | 2004


    Transient Spray Cone Angles in pressure-Swirl Injector Sprays

    Snyder, J. A. / Grover, R. O. / Sick, V. et al. | British Library Conference Proceedings | 2004


    Transient spray cone angles in pressure-swirl injector sprays

    Snyder,J.A. / Grover,R.O. / Sick,V. et al. | Kraftfahrwesen | 2004