A 3-D CFD analysis of the Space Shuttle RSRM with propellant fins @ 1s burn-back

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2003, Pages

  Morstadt, R A ^a  

^a NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

3-D MODELING; AXISYMMETRIC; BORE PRESSURES; CFD ANALYSIS; COUNTER ROTATING; REYNOLDS STRESS MODELS; TURBULENT MODELS;

COMPUTATIONAL FLUID DYNAMICS; FINS (HEAT EXCHANGE); FLOW PATTERNS; PRESSURE DROP; SOLID PROPELLANTS; SPACE SHUTTLES; SPACECRAFT PROPULSION;

THREE DIMENSIONAL;

EID: 84897585839     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

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2. Eaton, A. M., and Laubacher, B. A., "Simulation of the Reusable Solid Rocket Motor Flow Field Near Ignition, " 38th JANNAF Combustion Subcommittee, Destin, Florida, April, 2002.
3. Ahmad, R. A., Morstadt, R. A., Eaton, A. M., "RSRM and ETM-03 Internal Flow Simulations and Comparisons, " 39th AIAA Joint Propulsion Conference, AIAA paper no. 2003-5105, July 20-23, 2003.
4. Culick, F. E. C., "Rotational Axi-symmetric Mean Flow and Damping of Acoustic Waves in Solid Propellant Motors, " AIAA Journal, vol. 4, No. 8, pp. 1462-1464, 1966.
5. Chaouat, Bruno, "Flow Analysis of a Solid Propellant Rocket Motor with Aft Fins, " Journal of Propulsion and Power, Vol. 13, No. 2, pp. 194-196, March-April 1997.
6. Lamb, H., Hydrodynamics, 6th Ed., pp. 223-224, Dover Publications, N. Y., 1945.
7. Milne-Thomson, L. M., Theoretical Hydrodynamics, 4th Ed., p. 361, MacMillian & Co., N. Y., 1960.
8. Robertson, J. M., Hydrodynamics in Theory and Application, p. 133, Prentice-Hall, Inc., Englewood Cliffs, N. J., 1965.