Steady/transient plume-launcher interactions and progress towards particulate/surface layer modeling

33rd Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1995, Pages

  York, B J ^a   Sinha, N ^a   Dash, S M ^a   Anderson, L ^b   Gominho, L ^b   Koo, J H ^c   Cheung, F B ^d  

^a Syst Simulation Dvmt Directorate   (United States)

^b NAVAL SURFACE WARFARE CENTER   (United States)

^c LP   (United States)

^d PENNSYLVANIA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; EROSION; FLOW FIELDS; LAUNCHING; NAVIER STOKES EQUATIONS; SOLID PROPELLANTS; TWO PHASE FLOW;

AFTERBURNING; INTERACTION PROBLEMS; LAUNCHER SYSTEMS; LAYER MODEL; NAVIER-STOKES CODE; NON EQUILIBRIUM; PROTECTIVE MATERIALS; SOLID-PROPELLANT MOTORS;

ABLATIVE MATERIALS;

EID: 84963556576     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Sinha, N., Dash, S.M., and Hosangadi, A., "Applications of an Implicit, Upwind NS Code, CRAFT, to Steady/Unsteady Reacting, Multi-Phase Jet/Plume Flowfields," AIAA-92-0837, AIAA 30th Aerospace Sciences Meeting, Reno, NV, January 6-9, 1992.
2. Hosangadi, A., Sinha, N., York, B.J., and Dash, S.M., "Progress Towards the Analysis of Transient Combusting, Multiphase Flows Using Upwind/Implicit Numerics," AIAA-93-0238, 31st AIAA Aerospace Sciences Meeting, January 11-14, 1993.
3. Cooper, G. and Sirbaugh, J., "The PARC Distinction: A Practical Flow Simulator," AIAA Paper 902002, June 19902.
4. York, B.J., Sinha, N. and Dash, S.M., "Computational Models for Chemically-Reacting Hypersonic Flow," AIAA-88-0509, Reno, NV, Jan. 1988.
5. Sinha, N., York, B.J., and Dash, S.M., "Applications of a Generalized Implicit Navier-Stokes Code, PARCH, to Supersonic and Hypersonic Propulsive Flowfields," AIAA-88-3278, Boston, MA, July 1988.
6. York, B.J., Sinha, N., Ong, C.C., and Dash, S.M., "PARCH Navier-Stokes Reacting/Multiphase Analysis of Generalized Nozzle Flowfields," AIAA-89-1765, Buffalo, NY, June 1989.
7. Hosangadi, A., Sinha, N., Dash, S.M., "Solution of Two-Phase Dilute Gas Particle Mixtures Using Upwind Finite-Volume Methodology," AIAA-92-0344, AIAA 30th Aerospace Sciences Meeting, Reno, NV, January 6-9, 1992.
8. Dr. Leon Anderson private communication, Naval Surface Warfare Center, Dahigren, VA, May 1993.
9. Hermsen, R.W., "Aluminum Oxide Particle Size for Solid Rocket Motor Performance Predictions," J. Spacecraft, Vol. 18, No. 6, Nov.-Dec. 1981.
10. Henderson, J., "Thermal Model for the Prediction of Ablation Rates and Techniques for Measuring Thermal Conductivities of Composite Ablative Materials," Final Report, University of Rhode Island, Dept. of Mechanical Eng., Kingston, Rl, June 1, 1982.
11. Hosangadi, A., Sinha, N., and Dash, S.M., "CRAFT Code Solid Propellant ETC Gun Simulation via Lagrangian Fluidized Bed Extensions," JANNAF 31st Combustion Subcommittee Mtg., LMSC, Sunnyvale, CA, Oct. 17-21, 1994.