Progress in the simulation of particulate interactions in solid propellant rocket exhausts

37th Joint Propulsion Conference and Exhibit

Volumn , Issue , 2001, Pages

  York, B J ^a   Lee, R A ^a   Sinha, N ^a   Dash, S M ^a  

^a Syst Simulation Dvmt Directorate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DOMAIN DECOMPOSITION METHODS; LAGRANGE MULTIPLIERS; MISSILES; NAVIER STOKES EQUATIONS; PROPULSION; ROCKETS;

COMPUTATIONAL DOMAINS; NAVIER-STOKES CODE; PARALLEL DOMAIN DECOMPOSITION; PARTICULATE MOTION; PLUME INTERACTION; SOLID PROPELLANT ROCKET; STEADY-STATE PROBLEMS; UNSTRUCTURED GRID;

SOLID PROPELLANTS;

EID: 85088721182     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-3590     Document Type: Conference Paper

References (23)

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11. York, B.J., Sinha, N., Dash, S.M., Anderson, L., Gominho, L., Koo, J.H., and Cheung, F.B., "Steady/Transient Plume-Launcher Interactions and Progress Towards Particulate/Surface Layer Modeling," AIAA-95-0255, AIAA Aerospace Sciences Mtg., Reno, NV, January 9-12, 1995.
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15. York, B.J., Kenzakowski, D.C., Lee, R.A., Perrell, E.R., and Dash, S.M., "Particulate Simulation in Solid Propellant Rocket Exhaust Plumes," Final Technical Report No. CRAFTR-4/2000.008, April 2000.
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23. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 8-11, 2001.