Roh, Tae-Seong and Cohen, Norman S. and Beddini, Robert A. and Culick, Fred E. C. (1999) Numerical Analysis of Solid Rocket Motor Instabilities With AP Composite Propellants. AIAA Papers, AIAA-99-2804. American Institute of Aeronautics and Astronautics . http://resolver.caltech.edu/CaltechAUTHORS:20101118-132511549
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A non-steady model for the combustion of ammonium perchlorate composite propellants has been developed in order to be incorporated into a comprehensive gasdynamics model of solid rocket motor flow fields. The model including the heterogeneous combustion and turbulence mechanisms is applied to nonlinear combustion instability analyses. This paper describes the essential mechanisms and features of the model and discusses the methodology of non-steady calculations of the combustion instabilities of solid rocket motors.
|Item Type:||Report or Paper (Technical Report)|
|Additional Information:||©1999 by the authors. This work has been partially supported by the Caltech Multidisciplinary University Research Initiative under ONR Grant No. N00014-95-1-1338; Dr. Judah Goldwasser of the Office of Naval Research is Program Manager.|
|Group:||Guggenheim Jet Propulsion Center, GALCIT|
|Other Numbering System:|
|Official Citation:||Numerical analysis of solid rocket motor instabilities with AP composite propellants Roh, Tae-Seong, California Inst. of Technology, Pasadena; Culick, Fred E. C., California Inst. of Technology, Pasadena; Cohen, Norman S., Cohen Professional Services, Redlands, CA; Beddini, Robert A., Illinois, Univ., Urbana AIAA-1999-2804 AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 35th, Los Angeles, CA, June 20-24, 1999|
|Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Ruth Sustaita|
|Deposited On:||18 Nov 2010 21:56|
|Last Modified:||22 Sep 2016 21:52|
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