Unsteady-state rocket nozzle flows

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2002, Pages

  Chang, I Shih ^a  

^a AEROSPACE CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW FIELDS; MESH GENERATION; PROPULSION; ROCKETS;

INLET CONDITIONS; SALIENT FEATURES; SOLID ROCKET MOTORS; SPACE-TIME CONSERVATION ELEMENT; STEADY-STATE FLOWS; SUBMERGED NOZZLES; UNSTEADY-STATE FLOW; UNSTRUCTURED MESHES;

ROCKET NOZZLES;

EID: 85087599519     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-3884     Document Type: Conference Paper

References (13)

1. Anon., "Titan IVB-24 Post-Flight Report-Flight Test Objectives/Performance Analysis, " MCR-0012-0204, Lockheed-Martin Astronautics, April 8, 1997.
2. Chang, S. C., "The Method of Space-Time Conservation Element and Solution Element-A New Approach for Solving the Navier-Stokes and Euler Equations, " J. Comput. Phys., 1995, pp. 295-324.
3. Chang, S. C., X. Y. Wang, and C. Y. Chow, "The Space-Time Conservation Element and Solution Element Method-A New High-Resolution and Genuinely Multidimensional Paradigm for Solving Conservation Laws, " J. Comput. Phys., 1999, pp. 89-136.
4. Chang, S. C., S. T. Yu, A. Himansu, X. Y. Wang, C. Y. Chow, and C. Y. Loh, "The Method of Space-Time Conservation Element and Solution Element-A New Paradigm for Numerical Solution of Conservation Laws, " Computational Fluid Dynamics Review 1998, Vol. 1, pp. 206-240, World Scientific, Singapore, publ.
5. Wang, X. Y. and S. C. Chang, "A 2D Non-Splitting Unstructured Triangular Mesh Euler Solver Based on the Space-Time CE/SE Method, " Computational Fluid Dynamics J., 1999, pp. 309-325.
6. Wang, X. Y., S. C. Chang, and P. C. E. Jorgenson, "Prediction of Sound Waves Propagating Through a Nozzle Without/With Shock Waves Using the Space-Time CE/SE Method, " AIAA Paper 2000-0222, presented at the 38th AIAA Aerospace Science Meeting, January 10-13, 2000, Reno, Nevada.
7. Loh, C. Y., L. S. Hultgren, S. C. Chang, and P. C. E. Jorgenson, "Aeroacoustics Computation for Nearly Fully Expanded Supersonic Jets Using the CE/SE Method, " AIAA Paper 2000-2010, presented at the sixth AIAA/CEAS Aeroacoustics Conference, June 12-14, 2000, Maui, Hawaii.
8. Yu, S. T., S. C. Chang, P. C. E. Jorgenson, S. J. Park, and M. C. Lai, "Treating Stiff Source Terms in Conservation Laws by the Space-Time CE/SE Method, " Proceedings of the 16th International Conference on Numerical Method in Fluid Dynamics, Arcachon, France, July 6-July 10, 1998.
9. Chang, I-Shih, "An Efficient, Intelligent Solution for Viscous Flows Inside Solid Rocket Motors, " AIAA 27th Joint Propulsion Conf., Sacramento, CA, Paper 91-2429, June 1991; also 1990 JANNAF Propulsion Meeting, Anaheim, CA, CPIAPUB-550, Vol. II, pp. 47-61, Oct. 1990.
10. Chang, I-Shih, "Adaptive, Unstructured, Finite-Element, Multimaterial, Thermal Analysis, " AIAA J. of Spacecraft and Rockets, Vol. 30, No. 1, pp. 43-50, Jan. 1993.
11. Chang, I-Shih, "One-and Two-Phase Nozzle Flows, " AIAA J., Vol. 18, No 12, pp. 1455-1461, Dec. 1980; also AIAA 18th Aerospace Sciences Meeting, Pasadena, CA, Paper 80-0272, Jan. 1980.
12. Cuffel, R. F., L. H. Back, and P. F. Massier, "Transonic Flowfield in a Supersonic Nozzle with Small Throat Radius of Curvature, " AIAA J., Vol. 7, No. 7, July 1969, pp. 1364-1366.
13. Chang, I-Shih, N. R. Patel, and S. H. Yang, "Titan IV Motor Failure and Redesign Analyses, " AIAA J. of Spacecraft and Rockets, Vol. 32, No. 4, pp. 612-618, July-Aug. 1995.