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Conjugate Calculation of Gas Turbine Vanes Cooled with Leading Edge Films 被引量:2
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作者 董平 王强 +2 位作者 郭兆元 黄洪雁 冯国泰 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2009年第2期145-152,共8页
Conjugate calculation methodology is used to simulate the C3X gas turbine vanes cooled with leading edge films of 'shower- head' type. By comparing calculated results of different turbulence models with the me... Conjugate calculation methodology is used to simulate the C3X gas turbine vanes cooled with leading edge films of 'shower- head' type. By comparing calculated results of different turbulence models with the measured data, it is clear that calculation with the transition model can better simulate the flow and heat transfer in the boundary layers with leading edge film cooling. In the laminar boundary layers, on the upstream suction side, the film cooling flow presents 3D turbulent characteristics before tran... 展开更多
关键词 gas turbine conjugate calculation leading edge film cooling TRANSITION temperature gradient
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Conjugate calculation of a film-cooled blade for improvement of the leading edge cooling configuration 被引量:3
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作者 Norbert Moritz Karsten Kusterer +3 位作者 Dieter Bohn Takao Sugimoto Ryozo Tanaka Tomoki Taniguchi 《Propulsion and Power Research》 SCIE 2013年第1期1-9,共9页
Great efforts are still put into the design process of advanced film-cooling configurations.In particular,the vanes and blades of turbine front stages have to be cooled extensively for a safe operation.The conjugate c... Great efforts are still put into the design process of advanced film-cooling configurations.In particular,the vanes and blades of turbine front stages have to be cooled extensively for a safe operation.The conjugate calculation technique is used for the three dimensional thermal load prediction of a fim-cooled test blade of a modern gas turbine.Thus,it becomes possible to take into account the interaction of internal flows,external flow,and heat transfer without the prescription of heat transfer ooefficients.The focus of the investigation is laid on the leading edge part of the blade.The numerical model consists of all internal flow passages and cooling hole rows at the leading edge.Furthermore,the radial gap flow is also part of the model.The comparison with thermal pyrometer measurements shows that with respect to regions with high thermal load a qualitatively and quantitatively good agreement of the conjugate results and the measurements can be found.In particular,the region in the vicinity of the mid-span section is exposed to a higher thermal load,which requires further improvement of the cooling arrangement.Altogether the achieved results demonstrate that the conjugate calculation technique is applicable for reasonable prediction of three-dimensional thermal load of complex cooling configurations for blades. 展开更多
关键词 Gas turbine Rotor blade Film-cooling conjugate heat transfer conjugate calculation Pyrometer measurement
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A Fast Bayesian Evaluation Algorithm Based on the Second Category of Maximum Likelihood
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作者 孟晶 郑榕 刘君 《Journal of Donghua University(English Edition)》 EI CAS 2015年第2期305-309,共5页
Directing at evaluation for qualifying rate in weaponry test,this article discusses firstly how field test information is flooded with lots of prior information.Then a fast Bayesian evaluation algorithm is presented b... Directing at evaluation for qualifying rate in weaponry test,this article discusses firstly how field test information is flooded with lots of prior information.Then a fast Bayesian evaluation algorithm is presented based on the elaborate analysis of prior information reliability and the second category of maximum likelihood.The example demonstrates that the algorithm presented in this article is better and more robust compared with classical evaluation algorithm for safe-or-failure test and normal Bayesian method,which can make the best of prior information. 展开更多
关键词 Bayesian prior Likelihood likelihood elaborate conjugate applying calculating confidence consistency
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