Integrated aerodynamic design and analysis of turbine blades

Talya, 2000, Multidisciplinary optimization for gas turbine airfoil design, Inverse Problems Eng, 8, 283, 10.1080/174159700088027731 Joubert H, Quiniou H, Turbomachinery design used intensive CFD. 22nd Congress of International Council of the Aeronautical Sciences. 28 August – 1st September, 2000, Harrogate, UK. Wang, 2002, An integration architecture for process manufacturing systems, Int J Comput Integr Manuf, 15, 413, 10.1080/09511920110118768 He W, Xu L. Integration of distributed enterprise applications: a survey, IEEE Transactions on Industrial Informatics, 2013 http://dx.doi.org/10.1109/TII.2012.2189221. Talya SS, Chattopadhya A, Rajadas JN. An integrated multidisciplinary design optimization procedure for cooled gas turbine blades. In: 41st AIAA/ASME/ASCE/AHS/ASG Structures, Structural Dynamics, and Materials Conference and Exhibit, Atlanta, GA, USA, 3-6 April 2000. Houstis, 2002, GasTurbnLab: a multidisciplinary problem solving environment for gas turbine engine design on a network of nonhomogeneous machines, J Comput Appl Math, 149, 83, 10.1016/S0377-0427(02)00522-8 Koini, 2009, A software tool for parametric design of turbomachinery blades, Adv Eng Software, 40, 41, 10.1016/j.advengsoft.2008.03.008 Qiu, 2010, An integrated design system for turbomachinery, J Hydrodynamics, 22, 358, 10.1016/S1001-6058(09)60219-5 Wang C. Insights into developing an MDO environment for complex engineering systems. Journal of Engineering Design. Submitted for review. Wang C. Multidisciplinary engineering application integration based on component technology. In: Maropoulos PG, Newman Stephen T editors. Proceedings of the 4th international conference on digital enterprise technology. Bath UK. 19–21 September, 2007; p. 185–92 Wang, 2008, Parameter mapping and data transformation for engineering application integration, Inf Sys Frontier, 10, 589, 10.1007/s10796-008-9112-5 Wang, 2012, Advances in information integration infrastructures supporting multidisciplinary design optimization, Enterprise Inf Sys, 6, 265, 10.1080/17517575.2011.653833 Feng, 2009, Integrated data management in complex product collaborative design, Comput Ind, 60, 48, 10.1016/j.compind.2008.09.006 Huang, 2009, A robust archived differential evolution algorithm for global optimization problems, J Comput, 4, 160, 10.4304/jcp.4.2.160-167 Huang, 2011, Optimal design of aeroengine turbine disc based on kriging surrogate models, Comput Struct, 89, 27, 10.1016/j.compstruc.2010.07.010 Yu, 2010, A CAE-integrated distributed collaborative design system for finite element analysis of complex product based on SOOA, Adv Eng Software, 41, 590, 10.1016/j.advengsoft.2009.11.006 Xu, 2012, Using propositional logic for requirements verification of service workflow, IEEE Trans Ind Inf, 6, 639, 10.1109/TII.2012.2187908 Lwin, 2012, A distributed web-based framework for helicopter rotor blade design, Adv Eng Software, 53, 14, 10.1016/j.advengsoft.2012.07.003 Tournier, 2010, Axial flow, multi-stage turbine and compressor models, Energy Convers Manage, 51, 16, 10.1016/j.enconman.2009.08.005 Denton, 1999, Computational fluid dynamics for turbomachinery design, Proc Inst Mech Eng J Mech Eng Sci. Part C, 107 Ristic, 2004, Measurement-based updating of turbine blade CAD models: a case study, Int J Comp Integr Manuf, 17, 352, 10.1080/0951192032000159148 Hoschek, 2000, Turbine blade design by lofted B-spline surfaces, J comput Appl Math, 119, 235, 10.1016/S0377-0427(00)00381-2 Hearn D, Baker MP, Carithers WR. Computer Graphics with OpenGL. 4th ed. Pearson Education Asia Ltd. and Publishing House of, Electronics Industry; 2012. Wei N. Significance of loss models in aerothermodynamic simulation for axial Turbines. Doctoral Thesis, Department of Energy Technology, Division of Heat and Power Technology, Royal Institute of Technology, Sweden, 2000.