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Volume : II, Issue : VII, August - 2012 Optimization Of Gas Turbine Blades K.Chandrasekhar, M.Ananda Rao and B.Sudheer prem kumar DOI : 10.9780/22307850, Published By : Laxmi Book Publication Abstract : This study is part of research project concerning the development of High Pressure
turbine blades with advanced cooling systems. Due to the high gas temperatures
entering the turbine of the most recent aero-engines in general up to 2000 K at the
turbine inlet at 40 bars, a very efficient cooling system is required in order to maintain
the metal temperatures below the allowable limits. This means to use a certain amount of
"cold" air directly extracted from the compressor, with a significant negative impact on
the engine performance.
A novel methodology has been used to design the layout of the tip cooling nozzles of a
high pressure rotor blade turbine. The methodology used is through a complete CAE
approach, by means of a parametric CFD model which is run many times for the
exploration of several designs by an optimizer. Keywords : Article : Cite This Article : K.Chandrasekhar, M.Ananda Rao and B.Sudheer prem kumar, (2012). Optimization Of Gas Turbine Blades. Indian Streams Research Journal, Vol. II, Issue. VII, DOI : 10.9780/22307850, http://oldisrj.lbp.world/UploadedData/1256.pdf References : - D.Sindar, B.Umadevi and Dr.K.Alagarsamy, “ Multi Objective Genetic Algorithm for the Optimized Resource Usage and the Prioritization of the Constraints in the Software Project Planning”. International Journal of Computer Applications (0975 – 8887), Volume 3 – No.3, June 2010
- . Behrooz Farshi*, Reza Taghavi-Zenouz, Saeed Mirshamsi Iran University of Science & Technology, Mechanical Engineering Department,“Preliminary Design optimization of Axial Compressors” Iranian Journal of Mechanical Engineering Vol. 5, No. 1, August 2004
- A. Keskin and D. Bestle. Application of Multi-Objective Optimization to Axial Compressor Preliminary Design. DGLR Jahrestagung, DGLR-2005-192, 2005.
- . M. A. Trigg, G. R. Tubby, and A. G. Shreard. Automatic Genetic Optimization Approach to Two- Dimensional Blade Pro¯le Design for Steam Turbines. Journal of Turbomachinery, ASME, Vol. 121:11{17, 1999.
- U. Koeller, R. Moenig, B. Kuesters, and H.-A. Schreiber. Development of Advanced Com- pressor Airfoils for Heavy-Duty Gas Turbines - Part I: Design and Opimization. Journal of Turbomachinery, ASME, Vol. 122:397{405, 2000.
- . F. Sieverding, B. Ribi, M. Casey, and M. Meyer. Design of Industrial Axial Compressor Blade Sections for Optimal Range and Performance. Journal of Turbomachinery ASME, Vol. 126:323{331, 2004.
- D. Bueche, G. Guidati, and P. Stoll. Automated Design Optimization of Compressor Blades for Stationary, Large-Scale Turbomachinery. Proceedings of ASME Turbo Expo 2003, GT2003-38421, 2003.
- . D.Bestle. Analyse und Optimierung von Mehrkoerpe
- Alternative Approach for Solving a Multi-Objective Optimization Problem in Aerodynamic Compressor Blade Design” - A. Keskin¤, A. K. Dutta and D. Bestle Brandenburg University of Technology Cottbus Chair of Engineering Mechanics and Vehicle Dynamics D-03013 Cottbus, Germany
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