Validation of analytical and time-accurate computational side load models for over-expanded flows in rocket nozzles

Proceedings of the International Conference on Parallel and Distributed Processing Techniques and Applications

Volumn 3, Issue , 2003, Pages 1305-1311

  Schwane, Richard ^a   Xia, Yang ^a  

^a ESTEC Eur Space Agy Atos Origin   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; NAVIER STOKES EQUATIONS; NOZZLES; STEADY FLOW; WIND TUNNELS;

FORCED HARMONIC MOTION; OVER-EXPANDED FLOW; SEPARATED FLOW;

AERODYNAMICS;

EID: 1642273980     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. L.-O. Pekkari, "Aeroelastic Analysis of Side Load in Supersonic Nozzles with Separated Flow", AIAA-94-3377, 30th AIAA/ASEM/SAE/ASEE Joint Propulsion Conference, Indianapolis, IN, June 27-29, 1994.
2. M. Frey, "Behandlung von Strömungsproblemen in Raketendüsen bei Überexpansion", PhD Thesis, Universität Stuttgart, Germany, 2001.
3. R. Schmucker, "Strömungsvorgänge beim Betrieb Überexpandierter Düsen Chemischer Raketentriebwerke", Technical University, Rept. TB-7, -10, -14, Munich, July 1973.
4. S. Deck and Ph. Guillen, "Numerical Simulation of Side Loads in an Ideal Truncated Nozzle", Journal of Propulsion and Power, Vol. 18, No. 2, pp. 261-269.
5. R. Schwane, H. Wong, and L. Toerngren, "Validation of Unsteady Turbulent Flow Predictions for Over-Expanded Expansion Nozzles". Proceedings of ICCFD2, Sidney, Australia July 15-19, 2002.
6. L. Toerngren, "Correlation between Outer Flow and Internal Nozzle Pressure Fluctuations", Proceedings of the 4th European Symposium on Aerothermodynamics for Space Vehicles, Capua, Italy, 15-18 October, 2001.
7. W.J. Coirier, Y. Jiang, D.M. Fricker, I. Haq, A.J. Przekwas, V.J. Harrand, and A.K. Singhal, "An Unstructured Parallel Solution Adaptive Simulation System for CFD and Multidisciplinary Analysis", AIAA 14th CFD Conference, July 1999.
8. R. Schwane, G. Hagemann, and P. Reijasse, "Plug Nozzles: Assessment of Prediction Methods for Flow Features and Engine Performance", AIAA Paper 2002-0585.
9. S. Herget, "Critical Evaluation of CFD Turbulence Models in Unsteady Flow", Diploma Thesis, 2000.
10. B. Baldwin and H. Lomax, "Thin-Layer Approximation and Algebraic Model for Separated Turbulent Flows", AIAA-78-257, AIAA 16th Aerospace Sciences Meeting, Huntsville, Alabama, January 16-18, 1978.
11. W. Kwan and R. Stark, "Flow Separation Phenomena in Subsonic Rocket Nozzles", AIAA-2002-4229, Indianapolis 2002.