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Cites:

Information Journal Paper

Title

DUAL BASE SWIRL INJECTOR DESIGN FOR INCREASING SPECIFIC IMPLUSE IN A LIQUID-FUEL ROCKET ENGINE

Pages

  11-21

Abstract

 In this article, the fundamental calculations of swirl injectors were investigated and the design method for these kinds of injector, i.e. dual-base liquid-liquid injectors, was presented based on this theory and some experimental results. Then, some special conditions related to dual based liquid-liquid injectors were studied and the corresponding results were considered in the design manipulation. The behavior of injector in various performing conditions and mutual effects on twin spray envelopes in dual base injector were investigated, and the design procedure was presented based on the obtained results. Finally, the computer code for designing this type of injector was proposed. Using this code, some injectors were designed and tested. The results were satisfactory.

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  • Cite

    APA: Copy

    OMI, F., MOVAHEDNEZHAD, E., & KARGAR, A.. (2007). DUAL BASE SWIRL INJECTOR DESIGN FOR INCREASING SPECIFIC IMPLUSE IN A LIQUID-FUEL ROCKET ENGINE. AEROSPACE MECHANICS JOURNAL, 3(1), 11-21. SID. https://sid.ir/paper/101716/en

    Vancouver: Copy

    OMI F., MOVAHEDNEZHAD E., KARGAR A.. DUAL BASE SWIRL INJECTOR DESIGN FOR INCREASING SPECIFIC IMPLUSE IN A LIQUID-FUEL ROCKET ENGINE. AEROSPACE MECHANICS JOURNAL[Internet]. 2007;3(1):11-21. Available from: https://sid.ir/paper/101716/en

    IEEE: Copy

    F. OMI, E. MOVAHEDNEZHAD, and A. KARGAR, “DUAL BASE SWIRL INJECTOR DESIGN FOR INCREASING SPECIFIC IMPLUSE IN A LIQUID-FUEL ROCKET ENGINE,” AEROSPACE MECHANICS JOURNAL, vol. 3, no. 1, pp. 11–21, 2007, [Online]. Available: https://sid.ir/paper/101716/en

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