1. 1Lee,S.Y.,andKim,K.Y."DesignOptimizationof Axial Flow Compressor Blades with a Three-Dimensional Navier-Stokes Solver, Proceedings of the ASME TurboExpo2000,Munich,Germany,May8-11,2000.
2. 2Janus,J.M.,andNewman,J.C."Aerodynamicand Thermal Design Optimization for Turbine Airfoils," AIAAPaperNo.2000-0840,39thAIAAAerospaceSci-enceMeetingandExhibit,Reno,NV,Jan.8-11,2001.
3. 3Rai, M. M. "A Rapid Aerodynamic Design ProcedureBasedonArtificialNeuralNetworks,"AIAAPaper No.2001-0315,Jan.2001.
4. 4Pierret, S., and Braembussche, R. A. V. "Turbomachinery Blade Design Using a Navier-Stokes Solver and Artificial Neural Network," Journal of Turbomachinery, Vol121,No.4,pp.326-332,1999.
5. 5Papila, N., Shyy, W., Griffin, L. W., and Dorney, D. J. "Shape Optimization of Supersonic Turbines Using Response Surface and Neural Network Methods," AIAAPaperNo.2001-1065,Jan.2001.