Aerostructural optimization of a transonic compressor rotor

Journal of Propulsion and Power

Volumn 22, Issue 4, 2006, Pages 880-888

  Lian, Yongsheng ^a,c,d,e   Liou, Meng Sing ^b,e,f  

^a OHIO AEROSPACE INSTITUTE   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

^c University of Michigan ^*  (United States)

^d UNIVERSITY OF MICHIGAN   (United States)

^e AIAA   (United States)

^f MS 5 11   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COMPRESSORS; COMPUTATIONAL METHODS; COMPUTER SOFTWARE; COUPLINGS; FINITE ELEMENT METHOD; INTERPOLATION; NAVIER STOKES EQUATIONS; OPTIMIZATION; STRUCTURAL ANALYSIS; TRANSONIC AERODYNAMICS;

AEROSTRUCTURAL OPTIMIZATION; COMPUTATIONAL TIME; STRUCTURE DYNAMICS; TRANSONIC COMPRESSOR BLADE; TRANSONIC COMPRESSOR ROTOR;

ROTORS;

EID: 33746881086     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.15397     Document Type: Article

References (27)

1. Oyama, A., Liou, M. S., and Obayashi, S., "Transonic Axial-Flow Blade Shape Optimization Using Evolutionary Algorithm and Three-Dimensional Navier-Stokes Solver," Journal of Propulsion and Power, Vol. 20, No. 4, 2004, pp. 612-619.
2. Benini, E., "Three-Dimensional Multi-Objective Design Optimization of a Transonic Compressor Rotor," Journal of Propulsion and Power,.Vol 20, No. 3, 2004, pp. 559-565.
3. Mengistu, T., and Ohaly, W., "Single and Multipoint Shape Optimization of Gas Turbine Blade Cascades," AIAA Paper 2004-4446, Aug.-Sept. 2004.
4. Lian, Y., and Liou, M. S., "Multiobjective Optimization Using Coupled Response Surface Model and Evolutionary Algorithm," AIAA Paper 2004-4323, Aug.-Sept. 2004;
5. also AIAA Journal, Vol. 43, No. 6, 2005, pp. 1316-1325.
6. Chamis, C. C., "Coupled Multidisciplinary Optimization of Engine Structural Performance," Journal of Aircraft, Vol. 36, No. 1, 1999, pp. 190-199.
7. Sobieszczanski-Sobieski, J., and Haftka, R. T., "Multidisplinary Aerospace Design Optimization: Survey of Recent Development," Structural Optimiation, Vol. 14, No. 1, 1997, pp. 1-23.
8. Deb, K., Multi-Objective Optimization Using Evolutionary Algorithms, Wiley, New York, 2001.
9. Borland, C. J., Benton, J. R., Frank, P. D., Kao, T. J., Mastro, R. A., and Barthelemy, J.-F., "Multidisciplinary Design Optimization of a Commercial Aircraft Wing-An Exploratory Study," AIAA Paper 94-4305-CP, Sept. 1994.
10. Martins, J. R. R. A., Alonso, J. J., and Reuther, J. J., "High-Fidelity Aerostructural Design Optimization of a Supersonic Business Jet," Journal of Aircraft, Vol. 41, No. 3, 2004, pp. 523-530.
11. Giunta, A. A., "A Novel Sensitivity Analysis Method for High Fidelity Multidisciplinary Optimization of Aerostructural Systems," AIAA Paper 2000-0683, Jan. 2000.
12. Maute, K., Nikbay, M., and Farhat, C., "Coupled Analytical Sensitivity Analysis and Optimization of Three-Dimensional Nonlinear Aeroelastic Systems," AIAA Journal, Vol. 39, No. 11, 2001, pp. 2051-2061.
13. Arnone, A., "Viscous Analysis of Three-Dimensional Rotor Flow Using a Multigrid Method," Journal of Turbomachinery, Vol. 116, No. 3, 1994, pp. 435-445.
14. Arnone, A., Liou, M. S., and Povinelli, L. A., "Navier-Stokes Solution of Transonic Cascade Flow Using Non-Periodic C-Type Grids," Journal of Propulsion and Power, Vol. 8, No. 2, 1992, pp. 410-417.
15. Friedmann, P. P., "Helicopter Vibration Reduction Using Structural Optimization with Aeroelastic/Multidisciplinary Constraints A Survey," Journal of Aircraft, Vol. 28, No. 1, 1991, pp. 8-21.
16. Chattopadhyay, A., and McCarthy, T. R., "A Multidisciplinary Optimization Approach for Vibration Reduction in Helicopter Rotor Blades," Journal of Computers and Mathematics with Applications, Vol. 25, No. 2, 1993, pp. 59-72.
17. Yuan, K.-A., and Friedmann, P. P., "Structural Optimization for Vibration Reduction of Composite Helicopter Rotor Blades with Advances Geometry Tips Subject to Multidisciplinary Constraints," Proceedings of the American Helicopter Society 51st Annual Forum, May 1995, pp. 937-956.
18. Livne, E., and Li, W.-L., "Aeroservoelastic Aspects of Wing/Control Surface Planform Shape Optimization," AIAA Journal, Vol. 33, No. 2, 1995, pp. 302-311.
19. Walsh, J. L., Young, K. C., Pritchard, J. I., Adelman, H. M., and Mantay, W. R., "Integrated Aerodynamic/Dynamic/Structural Optimization of Helicopter Rotor Blades Using Multilevel Decomposition," NASA TP-3465, ARL Technical Report 518, Jan. 1995.
20. Smith, M. J., Hodges, D. H., and Cesnik, C. E. S., "Evaluation of Computational Algorithms Suitable for Fluid-Structure Interactions," Journal of Aircraft, Vol. 37, No. 2, 2000, pp. 282-294.
21. Duchon, J. P., "Splines Minimizing Rotation-Invariant Semi-Norms in Sobolev Spaces," Constructive Theory of Functions of Several Variables, edited by W. Schempp and K. Zeller, Springer-Verlag, Berlin, 1977, pp. 85-100.
22. Brown, S. A., "Displacement Extrapolation for CFD+CSM Aeroelastic Analysis," AIAA Paper 1997-1090, April 1997.
23. Liu, F., Cai, J., Zhu, Y., Tsai, H. M., and Wong, A. S. F., "Calculation of Wing Flutter by a Coupled Fluid-Structure Method," Journal of Aircraft, Vol. 38, No. 2, 2001, pp. 334-342.
24. Lian, Y., and Liou, M.S., "Multiobjective Optimization of a Transonic Compressor Rotor Using Evolutionary Algorithm," Journal of Propulsion and Power, Vol. 21, No. 6, 2005, pp. 979-987.
25. Beachkofski, B., and Grandhi, R., "Improved Distributed Hypercube Sampling," AIAA Paper 2002-1274, April 2002.
26. DOT User's Manual, ver. 4.20, Vanderplaats Research and Development, Inc., Colorado Springs, CO, 1995.
27. Bishop, C. M., Neural Network for Pattern Recognition, Oxford Univ. Press, 2003, pp. 187-189.