참고문헌
- Dunham, J., 1998, “CFD Validation for Propulsion System Components,” AGARD Advisory Report 355, ISBN 92-836-1075-X.
- Reid, L., and Moore, R. D., 1978, “Design and Overall Performance of Four Highly-Loaded, High-Speed Inlet Stages for anAdvanced, High-Pressure-Ratio Core Compressor,” NASA TP-1337.
- Samad, A., Kim, K. Y., Goel, T., Haftka, R. T., and Shyy, W., 2007, “Multiple Surrogate Modeling for Axial Compressor BladeShape Optimization,” Journal of Propulsion and Power, (Accepted for publication).
- Jang, C.M., and Kim, K.Y., 2007, “Applications of Numerical Optimization Techniques to Design of Axial CompressorBlades,” Journal of Aerospace Power, Vol. 22, No. 4, pp. 29-36.
- Yang, L., Ouyang, H., and Hui, D. Z., 2007, “Optimization Design and Experimental Study of Low-Pressure Axial Fan withForward-Skewed Blades,” International Journal of Rotary Machinery, Vol. 2007, Article ID 85275, 10 pages, doi:10.1155/2007/85275.
- Pierret, S., Coelho, R. F., and Kato, H., 2007, “Multidisciplinary and multiple operating points shape optimization of threedimensionalcompressor blades,” Structural and Multidisciplinary Optimization, Vol. 33, No. 1. pp. 61-70.
- Oyama, A., Liou, M.S., Obayashi, S., 2004, "Transonic Axial-Flow Blade Optimization: Evolutionary Algorithms/Three-Dimensional Navier-Stoke Solver,” Journal of Propulsion and Power, Vol. 20, No. 4, pp. 612-619. https://doi.org/10.2514/1.2290
- Chen, N., Zhang, H., Xu, Y., and Huang, W., 2007, “Blade Parameterization and Aerodynamic Design Optimization for a 3D Transonic Compressor Rotor,” Journal of Thermal Science, Vol. 16, No. 2, pp. 105-114. https://doi.org/10.1007/s11630-007-0105-3
- Chen, N.X., Zhang, H.W., Du, H., Xu, Y.J., and Huang, W.G., 2005, “Effect of Maximum Camber Location on AerodynamicPerformance of Transonic Compressor Blades,” ASME Turbo Expo 2005, Nevada, USA, GT2005-68541.
- Benini, E., 2004, “Three-Dimensional Multi-Objective Design Optimization of a Transonic Compressor Rotor,” Journal ofPropulsion and Power, Vol. 20, No. 3, pp. 559-565. https://doi.org/10.2514/1.2703
- Keskin, A. and Bestle, D., 2006, “Application of Multi-Objective Optimization to Axial Compressor Preliminary Design,”Aerospace Science and Technology, Vol. 10, pp. 581–589. https://doi.org/10.1016/j.ast.2006.03.007
- Wu, H., Li, Q. and Zhou, S., 2007, “Optimization of Loaded Fan Rotor Based on Through Flow Model,” ASME Turbo Expo,Montreal Canada, GT2007-27603.
- Sanger, N. L., 1983, “The Use of Optimization Techniques to Design-Controlled Diffusion Compressor Blading,” Journal ofEngineering for power, Vol. 105, pp. 256-264. https://doi.org/10.1115/1.3227410
- Queipo, N. V., Haftka, R.T., Shyy, W., Goel, T., Vaidyanathan, R. and Tucker, P.K., 2005, “Surrogate-based analysis andoptimization,” Progress in Aerospace Sciences, Vol. 41, pp. 1-28. https://doi.org/10.1016/j.paerosci.2005.02.001
- Li, W., and Padula, S., 2004, “Approximation Methods for Conceptual Design of Complex Systems,” Eleventh InternationalConference on Approximation Theory (eds. Chui, C., Neaumtu, M., Schumaker, L.).
- Goel, T., Haftka, R., Shyy, W., and Queipo, N., 2007, “Ensemble of Surrogates,” Structural and MultidisciplinaryOptimization, Vol. 33. No. 3, pp. 199-216. https://doi.org/10.1007/s00158-006-0051-9
- Samad, A., Shin, D. Y., Kim, K. Y., Goel, T., and Haftka, R. T., 2007, “Surrogate Modeling for Optimization of a DimpledChannel to Enhance Heat Transfer Performance,” Journal of Thermophysics and Heat Transfer, Vol. 21, No. 3, pp. 667-670. https://doi.org/10.2514/1.30211
- Ansys CFX-11.0, 2006, Ansys Inc.
-
Beheshti, B. H., Teixeira, J. A., Ivey, P.C., Ghorbanian, K., and Farhanieh, B., 2004, “Parametric Study of Tip ClearanceCasing Treatment on Performance and stability of a Transonic Axial Compressor,” Journal of turbomachinery, Vol. 126, pp. 527-535,
$JMP{\circledR}$ 5.1, 2004, SAS Institute, Inc. https://doi.org/10.1115/1.1791643 - Myers, R. H., and Montgomery, D. C., 1995, “Response Surface Methodology-Process and Product Optimization UsingDesigned Experiments,” John Wiley & Sons, Inc: New York.
- Orr, M. J. L., 1996, “Introduction to Radial Basis Neural Networks,” Center for Cognitive Science, Edinburgh University,Scotland, UK. http://anc.ed.ac.uk/rbf/.
- Martin, J. D., and Simpson, T. W., 2005, “Use of Kriging Models to Approximate Deterministic Computer Models,” AIAAJournal, Vol. 43, No. 4, pp. 853-863. https://doi.org/10.2514/1.8650
-
$MATLAB{\circledR}$ , The Language of Technical Computing, Release 14, 2004, The MathWorks Inc. - Guinta, A. A., 1997, “Aircraft Multidisciplinary Design Optimization Using Design of Experimental Theory and ResponseSurface Modeling Methods,” Ph. D. Dissertation, Department of Aerospace Engineering, Virginia Polytechnic Institute and StateUniversity, Blacksburg, VA.
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