Applications of an implicit, upwind Navier-Stokes code, CRAFT, to steady/unsteady reacting, multi-phase flowfields

Author:

SINHA N.1,DASH S.1,HOSANGADI A.1

Affiliation:

1. Science Applications International Corp., Fort Washington, PA

Publisher

American Institute of Aeronautics and Astronautics

Reference3 articles.

1. "Nickerson, G.R., Coats, D.E., and Hermsen, R.W. "Solid Propellant Rocket Motor Performance PredictionsUsingtheImprovedSPPComputerModel," "Seiner, J.M. Ponton,M.K.and Manning, J.C. "NASALaRCJetPlumeResearch," First AnnualHigh S& Research Workshou, Williamsburg, VA,May14-16,1991. 31Dash,S.M., Sinha, N., York, B.J. and Lee, R.A. "Progress in the Development of Advanced ComputationalModels for the Analysisof Generalized SupersonicJet Flowfields," AIAA 13thAeroAcoustics Conference, AIAA Paper 90-3915, Tallahassee, FL, October 1990. 3ZSinha,N., Dash, S.M., andYork, B.J. "Predictions ofJetMean-FlowSttuctureinSupportof HSCTNoise-SuppressionConcepts," ATAAISAIIASMEIASEE 27th Joint Prouulsion Conference. AIAA Paper 91-2253, Sacramento, CA, June 24-26, 1991. "Dash, S.M., Sinha, N., York, B.J., Kenzakowski, D.C., and Lee, R.A. "Computer Codes for HSCT Exhaust Flowfield Simulation and observations on Turbulence Modeling," 9th AIAA Applied Aerodynamics Conference, AIAA Paper 91-3297, Baltimore,MD, September 23-26, 1991. 34Dash,S.M. "Observationson Practical Turbulence ModelingforHigh-speedJetlPlumeFlowfields," AIAA 22nd Fluid and Plasmadynamics Conference, AIAA Paper 91.1789, Honolulu, Hawaii, June 24-26, 1991. "Dash, S.M., Walker, B.J., and Seiner, J.M."A Building-Block Approach for Turbulence Model ValidationlUpgrade Focussed on High-speed Jet Flows," to he presented at 1992JANNAF Prouulsion Meetin& Indianopolis,IN, February 24-28, 1992. %inha, N., A. Hosangadi, and Dash, S.M. "Simulationof ETC Gun Phenomena Using CRAFT ImplicitlUpwind Computer Code," 28th JANNAF CombustionMeeting, Brooks AFB, San Antonio,TX, Oct. 28 -Nov. 1, 1991. "Vinokur, M. "An Analysisof Finite-Differenceand Finite-VolumeFormulations of ConservationsLaws," NASA CR-177416,June 1986. '*A. Hosangadi and N. Sinha, "Development of a Dynamic Grid Navier-Stokes Solver for Computing Electro-Tbermo-Chemical Gun Configurations," SAIClFWTR-88, December 1990. '9Harten, A. Lax, P.D., and van-Leer, B. "On Upstream Differencingand Godunov-typeSchemes for HyperbolicConservationLaws,SIAM,Rev., 25(1983) pp.35-61. 40Collins, P. and Glaz, H.M. "Efficient Solution Algorithm for the Riemann Problem for Real Gases," J. Compurar.Physics, 59 (1985), pp. 264-298. 41Davis,S.F. "SimplifiedSecond-OrderGodunovType Methods," SIAM 1. Sci. Starit. Compur.,9 (1988)pp. 445-473. 42Bell, J.B., Colella, P. and Trangenstein, J.A. "Higher-OrderGodunovMethods for General System of Hyperbolic Conservation Laws, J. Cornputat. Physics, 82 (1989), pp. 362-397. 43Hosangadi, A. and York, B.J. "CRAFT Time DependentAnalysis of a Missile with Lateral Control Jet," prepared for US. Army Missile Command (MICOM),SAIClFWTM-67, November 1991. MYork, B.J., Sinha,N., Dash, S.M.,Anderson, L., Gominho, L. "Navier-Stokes Simulation of PlumelVertical Launching System Interaction Flowfields," AIAA 92-0839, AIAA 30th AerosDace SciencesMeeting, Reno, NV, January 6-9, 1992. x

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