Unsteady numerical simulations of the flow in a truncated ideal contour nozzle under free shock separation conditions

21st AIAA Applied Aerodynamics Conference

Volumn , Issue , 2003, Pages

  Schwane, Richard ^a   Perigo, David ^a,b   Xia, Yang ^a,b  

^a EUROPEAN SPACE AGENCY   (Netherlands)

^b ATOS ORIGIN BV   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FLOW STRUCTURE; PROPULSION; RIGID STRUCTURES; ROCKETS; SHOCK WAVES;

EXPERIMENTAL AND NUMERICAL STUDIES; EXTERNAL ENVIRONMENTS; LINEAR OSCILLATOR; NOZZLE CONFIGURATION; PRESSURE VARIATIONS; RIGID-BODY MOTION; SEPARATION CONDITION; UNSTEADY NUMERICAL SIMULATIONS;

ROCKET NOZZLES;

EID: 85067317875     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3676     Document Type: Conference Paper

References (14)

1. R. Eliasson, J. Nordstrom J.: The Development of an Unsteady Solver for Moving Meshes, FFA TN 1995-39
2. A. Jameson: Time Dependent Calculations using Multi-grid, with applications to Unsteady Flows Past Airfoils and Wings, AIAA-91-1596
3. H. Wong, R. Schwane: Numerical Investigation of Transition in Flow Separation in a Dual-bell Nozzle Proc. 4th European Symp. Aerothermodynamcis for Space Vehicles, Oct. 2001,Italy.
4. S. Herget: Critical Evaluation of CFD Turbulence Models in Unsteady Flows, Diploma Thesis, Munich Univ. of Technology TUM-FLM-2000/11 2000.
5. W. J. Coirier, Y. Jiang, D. M. Pricker, I. Haq, A, J. Przek-was, V. J. Harrand, A. K. Singhal: An Unstructured Parallel Solution Adaptive Simulation System for CFD and Multidisci-plinary Analysis AIAA 14th CFD Conference, July 1999.
6. R. Schwane, G. Hagemann, P. Reijasse: Plug Nozzles: Assessment of Prediction Methods for FLow Features and Engine Performance, AIAA 2002-0585
7. 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.
8. M. Prey, Behandlung von Strbmungsproblemen in Raketendiisen bei Uberexpansion, PhD Thesis, Universitat Stuttgart, Germany, 2001.
9. R. Schmucker, Stromungsvorgange beim Betrieb Uberexpandierter Diisen Chemischer Raketentriebwerke, Technical University Rept. TB-7, -10, -14, Munich, July 1973.
10. 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.
11. R. Schwane, H. Wong and L. Toerngren, Validation of Unsteady Turbulent Flow Predictions for Over-Expanded Expansion Nozzles. Proceedings of ICCPD2, Sidney, Australia July 15-19, 2002.
12. 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.
13. W. Kwan and R. Stark, Flow Separation Phenomena in Sub-sonic Rocket Nozzles, AIAA-2002-4229, Indianapolis 2002.
14. R. Schwane and Y. Xia: Validation of Analytical and Time-accurate Computational side-load Models for Over-expanded Rocket Nozzles, International Conference on Parallel and Distributed Processing Techniques and Applications, June 23-26, 2003, Las Vegas, Nv.