Improved aerodynamic design of turbomachinery bladings by numerical optimization

Aerospace Science and Technology

Volumn 7, Issue 4, 2003, Pages 277-287

  Burguburu, Stéphane ^a   Le Pape, Arnaud ^a  

^a ONERA   (France)

Author keywords

B zier; Compressor; Genetic; Gradient; Optimization; Turbomachinery

Indexed keywords

COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; DEFORMATION; DESIGN; EFFICIENCY; GENETIC ALGORITHMS; ITERATIVE METHODS; MACHINE DESIGN; NAVIER STOKES EQUATIONS; OPTIMIZATION; RELIABILITY; TURBOMACHINE BLADES;

SUCTION; TRANSONIC COMPRESSORS;

AERODYNAMICS;

EID: 0347604010     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(02)00010-X     Document Type: Article

References (17)

1. P. Bézier, Essais de définition numérique des courbes et surfaces expérimentales, Thèse de doctorat d'état, février 1977.
2. Bourdeau C., Carrier G., Knight D., Rasheed K. Three dimensional optimization of supersonics inlets. 35th AIAA - AIAA99-2108, Los Angeles, CA. June 1999.
3. Burguburu S., Toussaint C., Leroy G. Numerical optimization for turbomachinery blades aerodynamic design using a gradient method coupled with a Navier-Stokes solver. 15th ISABE, ISABE2001-1117, Bangalore, India. September 2001.
4. Chung J., Lee K.D. Shape optimization of transonic compressor blades using quasi-3D flow physics. ASME TURBOEXPO 2000-GT-0489 Munich, Germany. May 2000.
5. J. Chung, J. Shim, K.D. Lee, 3D design of transonic axial compressor blades with 3D Navier-Stokes physics, AIAA paper 2001-3305.
6. Couailler V. Numerical simulation of separated turbulent flows based on the solution of a RANS/low Reynolds two-equations model. 37th AIAA/ASME, Reno, USA. 1999.
7. Gummer V., Wenger U., Kau H.P. Using sweep and dihedral to control three-dimensional flow in transonic stator of axial compressor. ASME TURBOEXPO 2000-GT-0491, Munich, Germany. May 2000.
8. Samareh J.A. Multidisciplinary aerodynamic-structural shape optimization using deformation (MASSOUD). 8th AIAA/NASA/USAF/ISSMO Symposium on multidisciplinary analysis and optimization, Long beach, CA. September 2000.
9. Joubert H., Quiniou H. Turbomachinery design used intensive CFD. 22nd ICAS, HARROGATE. September 2000.
10. I. Le Madec, Modélisation des écoulements transitionnels et turbulents dans les grilles d'aubes de turbomachines suivant l'orientation turbines, Ph.D. thesis, Rennes University, 1993.
11. Liamis N., Couailler V. Unsteady Euler and Navier-Stokes simulations with an implicit Runge-Kutta method. Proceedings of 2nd European Computational Fluid dynamics Conference. 1994;Stuttgart, John Wiley.
12. Michel R., Quémard C., Durand R. Application d'un schéma de longueur de mélange à l'étude des couches limites turbulentes d'équilibre, Technical note 154. Office National d'Etudes et Recherches Aérospatiales. 1969.
13. W. Quinhuan, H. Xiaoyan, The use of Bézier polynomial patches to define geometrical shape of the flow channels of compressors, ASME 88-GT-60, 1988.
14. K. Rasheed, GADO: A genetic algorithm for continuous design optimization, Ph.D. thesis, Rutger, State University of New Jersey, January 1998.
15. Shaphar S. Three-dimensional design and optimization of turbomachinery blades using the Navier-Stokes equations. 15th ISABE, ISABE2001-1053, Bangalore, India. September 2001.
16. G.N. Vanderplaats, CONMIN - a fortran program for constrained function minimisation, NASA TMX 62282, 1973.
17. Vanderplaats G.N. Numerical Optimisation Techniques for Engineering Design with Applications, McGraw-Hill. 1984.