Closed-form analytical solutions for fluid mechanical, thermochemical, and thermal processes in solid rocket motors

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Salita, Mark ^a  

^a TRW SSTO   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLUID MECHANICS; NUMERICAL METHODS; PROPULSION; ROCKETS;

CLOSED FORM SOLUTIONS; CLOSED-FORM ANALYTICAL SOLUTIONS; COMPUTATIONAL PLATFORMS; DISCRETIZATION ERRORS; ENGINEERING ANALYSIS; FUNCTIONAL DEPENDENCE; NUMERICAL PREDICTIONS; NUMERICAL TECHNIQUES;

TWO PHASE FLOW;

EID: 85085407295     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-3965     Document Type: Conference Paper

References (19)

1. Salita, M, “Comparison of VOLFIL3 to an Exact Solution”, Thiokol memo 2814-FY85-M017, August 10, 1984.
2. Salita, M., “A Simple Computer Code (VOLS) for Predicting Filling/Discharge of Multiple Void Volumes in Series”, TRW IOC F321.MS.96-003, April 22,1996.
3. Shapiro, A.H., The Dynamics and Thermodynamics of Compressible Fluid Flow. Ronald Press, 1954.
4. Salita, M., “Verification of Spatial and Temporal Pressure Distributions in Segmented Solid Rocket Motors”, AIAA-89-0298, 27lh Aerospace Sciences Meeting, January 1989.
5. Culick, F.E.C., “Rotational Axisymmetric Mean Flow and Damping of Acoustic Waves in a Solid Propellant Rocket”, AIAAJ, Vol.4 No.8, August 1966, pp 1462-64.
6. Dunlap, R., Willoughby, P.O., and Hermsen, R.W., “Flowfield in the Combustion Chamber of a Solid Propellant Rocket Motor”, AIAAJ, Vol.2 No. 10, October 1974, pp 1440-42.
7. Dunlap, R., Blackner, A.M, Waugh, R.C., Brown, R.S., and Willoughby, P.O., “Internal Flowfield Studies in a Simulated Cylindrical Port Rocket Chamber”, Journal of Propulsion and Power, Vol.6 No.6, 1990, pp 690-704.
8. Salita, M., “VORSTREM: A Simple and Versatile 2D Viscous Solver for Chamber Flow in Solid Rocket Motors”, AIAA-94-0035, 30th Joint Propulsion Conference, June 1994.
9. McBride, B.J., Reno, M.A., and Gordon, S., “CET93 and CETPC: An Interim Updated Version of the NASA Lewis Computer Program for Calculating Complex Chemical Equilibria With Applications”, N AS ATM-4557, 1994.
10. Powars, C.A., and Kendall, R.M., “User’s Manual: Aerotherm Chemical Equilibrium (ACE) Computational Program”, Aerotherm Corporation, Mountain View, CA.
11. Cruise, D.R., “Theoretical Computations of Equilibrium Composition, Thermodynamic Properties, and Performance Characteristics of Propellant Systems”, NWC, TP-6037, ‘• November 1991.
12. Salita, M., “Understanding ACE Charring Thermochemistry Using the NASA Lewis Thermochemical Code or the 14-Species Simplified Model SIMPACE”, Thiokol TWR-40314, November 14, 1991.
13. Rogers, C.R., and Suh, N.P., “Ignition and Surface Temperatures of Double Base Propellants at Low Pressures II: Comparison of Optical and Thermocouple Techniques”, AIAAJ Vol.8 No.8, August 1970, pp 1501-1506.
14. Salita, M., “Predicted Slag Deposition Histories in Eight Solid Rocket Motors Using the CFD Model ‘EVT”, AIAA 95-2728, 31st Joint Propulsion Conference, July 1995.
15. Abramowitz, M., and Stegun, I.A., Handbook of Mathematical Functions. NBS, AMS #55, 8/66.
16. Pearce, B.E., “Radiative Heat Transfer Within a Solid-Propellant Rocket Motor”, J. Spacecraft, Vol.15 No.2, March 1978, pp 125-128.
17. Shadlesky, P., “Radiation from Absorbing, Scattering, and Emitting Media”, Thiokol memo 2815-82-M076, July 12,1982.
18. Salita, M., “Emissivity of Gas/Particle Clouds in Chambers of Solid Rocket Motors”, CPIA 557 (Vol I), 27th JANNAF Combustion Meeting, November 1990.
19. Salita, M., and Glatt, L., “Modeling of Ignition Overpressure in Minuteman Silos”, AIAA 97-2720, 33rd Joint Propulsion Conference, July 1997.