Moving extremum surrogate modeling strategy for dynamic reliability estimation of turbine blisk with multi-physics fields
To improve the dynamic reliability analysis of complex structures like turbine blisk, moving extremum surrogate modeling strategy (MESMS) is proposed in respect of multi-physics coupling with various dynamics/uncertainties. In this strategy, extremum thought is adopted to handle the dynamic process...
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| Published in | Aerospace science and technology Vol. 106; p. 106112 |
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| Main Authors | , , , , |
| Format | Journal Article |
| Language | English |
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Elsevier Masson SAS
01.11.2020
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| Subjects | |
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| Abstract | To improve the dynamic reliability analysis of complex structures like turbine blisk, moving extremum surrogate modeling strategy (MESMS) is proposed in respect of multi-physics coupling with various dynamics/uncertainties. In this strategy, extremum thought is adopted to handle the dynamic process of input parameters and output response, and the importance sampling (IS) method is utilized to extract efficient samples and improve the efficiency of dynamic reliability estimation, and moving least square (MLS) method is used to select good samples from training samples with local compact support region to establish a precise surrogate model. The dynamic reliability analysis of turbine blisk radial deformation with fluid-thermo-structural interaction is performed to validate the developed MESMS in approximate precision and simulation performance by comparing to other methods. As shown in this study, (i) the reliability degree of turbine blisk is 0.9975 when the allowable value of radial deformation is 2.6856 × 10−3 m subject to 3 sigma levels; (ii) the proposed MESMS processes high modeling accuracy and efficiency due to small error; (iii) the MESMS holds high simulation performance in efficiency and accuracy owing to outstanding computational consumption and simulation. These results demonstrate that the MESMS is effective and applicable in structural reliability estimation regarding dynamics and uncertainties. The efforts of this paper provide a useful insight for performing the reliability-based design optimization of complex structures besides turbine blisk. |
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| AbstractList | To improve the dynamic reliability analysis of complex structures like turbine blisk, moving extremum surrogate modeling strategy (MESMS) is proposed in respect of multi-physics coupling with various dynamics/uncertainties. In this strategy, extremum thought is adopted to handle the dynamic process of input parameters and output response, and the importance sampling (IS) method is utilized to extract efficient samples and improve the efficiency of dynamic reliability estimation, and moving least square (MLS) method is used to select good samples from training samples with local compact support region to establish a precise surrogate model. The dynamic reliability analysis of turbine blisk radial deformation with fluid-thermo-structural interaction is performed to validate the developed MESMS in approximate precision and simulation performance by comparing to other methods. As shown in this study, (i) the reliability degree of turbine blisk is 0.9975 when the allowable value of radial deformation is 2.6856 × 10−3 m subject to 3 sigma levels; (ii) the proposed MESMS processes high modeling accuracy and efficiency due to small error; (iii) the MESMS holds high simulation performance in efficiency and accuracy owing to outstanding computational consumption and simulation. These results demonstrate that the MESMS is effective and applicable in structural reliability estimation regarding dynamics and uncertainties. The efforts of this paper provide a useful insight for performing the reliability-based design optimization of complex structures besides turbine blisk. |
| ArticleNumber | 106112 |
| Author | Li, Huan Lu, Cheng Fei, Cheng-Wei An, Li-Qiang Liu, Hao-Tian |
| Author_xml | – sequence: 1 givenname: Cheng surname: Lu fullname: Lu, Cheng organization: Department of Aeronautics and Astronautics, Fudan University, Shanghai 200433, PR China – sequence: 2 givenname: Cheng-Wei orcidid: 0000-0001-5333-1055 surname: Fei fullname: Fei, Cheng-Wei email: cwfei@fudan.edu.cn organization: Department of Aeronautics and Astronautics, Fudan University, Shanghai 200433, PR China – sequence: 3 givenname: Hao-Tian surname: Liu fullname: Liu, Hao-Tian organization: Department of Aeronautics and Astronautics, Fudan University, Shanghai 200433, PR China – sequence: 4 givenname: Huan surname: Li fullname: Li, Huan organization: Department of Aeronautics and Astronautics, Fudan University, Shanghai 200433, PR China – sequence: 5 givenname: Li-Qiang surname: An fullname: An, Li-Qiang organization: Department of Mechanical Engineering, North China Electric Power University, Baoding 071003, PR China |
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| Cites_doi | 10.3390/ma12091545 10.1016/j.actaastro.2018.12.012 10.1016/j.tafmec.2016.05.004 10.1016/j.apm.2009.08.009 10.1016/j.ijhydene.2013.12.129 10.1016/j.cam.2015.01.007 10.2514/1.34321 10.1016/j.probengmech.2013.02.002 10.1016/j.ast.2019.105466 10.1016/S1000-9361(08)60044-8 10.1109/TR.2014.2313801 10.1090/S0025-5718-1981-0616367-1 10.1177/0954406211412319 10.1016/j.engfailanal.2019.104193 10.1016/j.ast.2018.02.012 10.1016/j.probengmech.2010.04.002 10.1016/j.ymssp.2016.05.026 10.1007/s00477-011-0517-1 10.2514/1.9255 10.1016/j.ast.2018.11.007 10.1177/0954406215607900 10.1109/TR.2019.2954379 10.1090/S0025-5718-98-00974-0 10.1016/j.apm.2017.02.047 10.1016/j.ast.2019.06.026 10.1016/j.strusafe.2016.02.002 10.1016/j.strusafe.2015.03.003 10.2514/1.I010045 10.3390/ma12152341 10.2514/1.A33801 10.1115/1.4030066 10.1016/j.ast.2012.11.010 10.1016/j.apnum.2015.07.006 10.1016/j.ast.2020.105906 10.1016/j.ast.2020.105788 |
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| Keywords | Dynamic reliability Radial deformation Turbine blisk Importance sampling method Moving extremum surrogate modeling strategy Fluid-thermal-structural interaction |
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| References | Zhang, Wei, Jing, Fei, Tang (br0320) 2019; 12 Lu, Feng, Liem, Fei (br0170) 2018; 76 Song, Bai, Fei, Tang (br0180) 2019; 92 Ou, Yan, Huang, Zhang (br0140) 2019; 155 Gao, Zio, Guo, Bai, Fei (br0080) 2020; 108 Kim, Lee, Paik, Lee (br0330) 2015; 55 Li (br0270) 2016; 99 Bichon, Eldred, Swiler, Mahadevan, McFarland (br0290) 2008; 46 Huang (br0100) 2014; 39 Fan, Li (br0340) 2008; 21 Dubourg, Sudret, Deheeger (br0300) 2013; 33 Fei, Bai, Tian (br0150) 2013; 10 Lu, Feng, Fei, Bu (br0380) 2020; 69 Lattime, Steinetz (br0010) 2004; 20 Hu, Yang, Fei (br0030) 2016; 30 Roshanian, Ebrahimi (br0260) 2013; 28 Zhai, Fei, Choy, Wang (br0230) 2017; 82 Lancaster, Salkauskas (br0200) 1981; 37 Groves, Bonello, Hai (br0070) 2012; 266 Kang, Koh, Choo (br0210) 2010; 25 Kim, Song, Kang (br0310) 2010; 34 Fei, Li, Liu, Lu, Keshtegar (br0370) 2020; 103 Ganji, Jowkarshorijeh (br0350) 2012; 26 Mirzaei (br0280) 2015; 282 Goswami, Ghosh, Chakraborty (br0220) 2016; 60 Levin (br0250) 1998; 64 Zhai, Fei, Wang, Yao (br0020) 2016; 230 Sankararaman, Daigle, Goebel (br0120) 2014; 63 Shen, Huang, Zhang, Yan (br0050) 2019; 84 Fei, Lu, Liem (br0190) 2019; 95 Zhang, Wang, Fei, Yuan, Wei, Tang (br0160) 2019; 12 Meguid, Maricic Luke (br0060) 2015; 137 Citarella, Giannella, Vivo, Mazzeo (br0090) 2016; 86 Shen, Huang, Yan, Zhang (br0040) 2020; 100 Keshtegar, Kisi (br0110) 2017; 48 Sun, Huang, Guo, Li (br0240) 2017; 54 Fei (10.1016/j.ast.2020.106112_br0190) 2019; 95 Levin (10.1016/j.ast.2020.106112_br0250) 1998; 64 Citarella (10.1016/j.ast.2020.106112_br0090) 2016; 86 Lu (10.1016/j.ast.2020.106112_br0170) 2018; 76 Groves (10.1016/j.ast.2020.106112_br0070) 2012; 266 Lancaster (10.1016/j.ast.2020.106112_br0200) 1981; 37 Ganji (10.1016/j.ast.2020.106112_br0350) 2012; 26 Lattime (10.1016/j.ast.2020.106112_br0010) 2004; 20 Hu (10.1016/j.ast.2020.106112_br0030) 2016; 30 Dubourg (10.1016/j.ast.2020.106112_br0300) 2013; 33 Sankararaman (10.1016/j.ast.2020.106112_br0120) 2014; 63 Fei (10.1016/j.ast.2020.106112_br0370) 2020; 103 Huang (10.1016/j.ast.2020.106112_br0100) 2014; 39 Gao (10.1016/j.ast.2020.106112_br0080) 2020; 108 Goswami (10.1016/j.ast.2020.106112_br0220) 2016; 60 Meguid (10.1016/j.ast.2020.106112_br0060) 2015; 137 Kim (10.1016/j.ast.2020.106112_br0330) 2015; 55 Shen (10.1016/j.ast.2020.106112_br0040) 2020; 100 Zhang (10.1016/j.ast.2020.106112_br0320) 2019; 12 Keshtegar (10.1016/j.ast.2020.106112_br0110) 2017; 48 Lu (10.1016/j.ast.2020.106112_br0380) 2020; 69 Ou (10.1016/j.ast.2020.106112_br0140) 2019; 155 Song (10.1016/j.ast.2020.106112_br0180) 2019; 92 Zhang (10.1016/j.ast.2020.106112_br0160) 2019; 12 Sun (10.1016/j.ast.2020.106112_br0240) 2017; 54 Fei (10.1016/j.ast.2020.106112_br0150) 2013; 10 Zhai (10.1016/j.ast.2020.106112_br0230) 2017; 82 Fan (10.1016/j.ast.2020.106112_br0340) 2008; 21 Roshanian (10.1016/j.ast.2020.106112_br0260) 2013; 28 Li (10.1016/j.ast.2020.106112_br0270) 2016; 99 Kim (10.1016/j.ast.2020.106112_br0310) 2010; 34 Shen (10.1016/j.ast.2020.106112_br0050) 2019; 84 Mirzaei (10.1016/j.ast.2020.106112_br0280) 2015; 282 Bichon (10.1016/j.ast.2020.106112_br0290) 2008; 46 Zhai (10.1016/j.ast.2020.106112_br0020) 2016; 230 Kang (10.1016/j.ast.2020.106112_br0210) 2010; 25 |
| References_xml | – volume: 95 year: 2019 ident: br0190 article-title: Decomposed-coordinated surrogate modelling strategy for compound function approximation and a turbine blisk reliability evaluation publication-title: Aerosp. Sci. Technol. – volume: 63 start-page: 603 year: 2014 end-page: 619 ident: br0120 article-title: Uncertainty quantification in remaining useful life prediction using first-order reliability methods publication-title: IEEE Trans. Reliab. – volume: 64 start-page: 1517 year: 1998 end-page: 1531 ident: br0250 article-title: The approximation power of moving least-squares publication-title: Math. Comput. – volume: 39 start-page: 3914 year: 2014 end-page: 3925 ident: br0100 article-title: Design exploration of three-dimensional transverse jet in a supersonic crossflow based on data mining and multi-objective design optimization approaches publication-title: Int. J. Hydrog. Energy – volume: 103 year: 2020 ident: br0370 article-title: Multilevel nested reliability-based design optimization with hybrid intelligent regression for operating assembly relationship publication-title: Aerosp. Sci. Technol. – volume: 20 start-page: 302 year: 2004 end-page: 311 ident: br0010 article-title: Turbine engine clearance control systems: current practices and future directions publication-title: J. Propuls. Power – volume: 86 start-page: 143 year: 2016 end-page: 152 ident: br0090 article-title: FEM-DBEM approach for crack propagation in a low pressure aeroengine turbine vane segment publication-title: Theor. Appl. Fract. Mech. – volume: 76 start-page: 164 year: 2018 end-page: 175 ident: br0170 article-title: Improved Kriging with extremum response surface method for structural dynamic reliability and sensitivity analyses publication-title: Aerosp. Sci. Technol. – volume: 34 start-page: 1225 year: 2010 end-page: 1237 ident: br0310 article-title: Stochastic approach to kinematic reliability of open-loop mechanism with dimensional tolerance publication-title: Appl. Math. Model. – volume: 48 start-page: 899 year: 2017 end-page: 910 ident: br0110 article-title: M5 model tree and Monte Carlo simulation for efficient structural reliability analysis publication-title: Appl. Math. Model. – volume: 84 start-page: 641 year: 2019 end-page: 649 ident: br0050 article-title: Parametric modeling and aerodynamic optimization of EXPERT configuration at hypersonic speeds publication-title: Aerosp. Sci. Technol. – volume: 21 start-page: 335 year: 2008 end-page: 340 ident: br0340 article-title: An efficient method for reliability-based multidisciplinary design optimization publication-title: Chin. J. Aeronaut. – volume: 266 start-page: 66 year: 2012 end-page: 81 ident: br0070 article-title: Efficient dynamic analysis of a whole aeroengine using identified nonlinear bearing models publication-title: Proc. Inst. Mech. Eng., Part C, J. Mech. Eng. Sci. – volume: 137 year: 2015 ident: br0060 article-title: Finite element modeling of shot peening residual stress relaxation in turbine disk assemblies publication-title: J. Eng. Mater. Technol. – volume: 60 start-page: 56 year: 2016 end-page: 66 ident: br0220 article-title: Reliability analysis of structures by iterative improved response surface method publication-title: Struct. Saf. – volume: 155 start-page: 287 year: 2019 end-page: 301 ident: br0140 article-title: Design exploration of combinational spike and opposing jet concept in hypersonic flows based on CFD calculation and surrogate model publication-title: Acta Astronaut. – volume: 12 start-page: 2341 year: 2019 ident: br0160 article-title: Fuzzy multi-SVR learning model for reliability-based design optimization of turbine blades publication-title: Materials – volume: 55 start-page: 70 year: 2015 end-page: 79 ident: br0330 article-title: Reliability assessment of reinforced concrete columns based on the P-M interaction diagram using AFOSM publication-title: Struct. Saf. – volume: 12 start-page: 1545 year: 2019 ident: br0320 article-title: Reliability-based low fatigue life analysis of turbine blisk with generalized regression extreme neural network method publication-title: Materials – volume: 33 start-page: 47 year: 2013 end-page: 57 ident: br0300 article-title: Metamodel-based importance sampling for structural reliability analysis publication-title: Probab. Eng. Mech. – volume: 92 start-page: 464 year: 2019 end-page: 477 ident: br0180 article-title: Multi-failure probabilistic design for turbine bladed disks using neural network regression with distributed collaborative strategy publication-title: Aerosp. Sci. Technol. – volume: 46 start-page: 2459 year: 2008 end-page: 2468 ident: br0290 article-title: Efficient global reliability analysis for nonlinear implicit performance functions publication-title: AIAA J. – volume: 69 start-page: 440 year: 2020 end-page: 457 ident: br0380 article-title: Improved decomposed-coordinated Kriging modeling strategy for dynamic probabilistic analysis of multi-component structures publication-title: IEEE Trans. Reliab. – volume: 100 year: 2020 ident: br0040 article-title: Constraint-based parameterization using FFD and multi-objective design optimization of a hypersonic vehicle publication-title: Aerosp. Sci. Technol. – volume: 37 start-page: 141 year: 1981 end-page: 158 ident: br0200 article-title: Surfaces generated by moving least squares methods publication-title: Math. Comput. – volume: 82 start-page: 323 year: 2017 end-page: 338 ident: br0230 article-title: A stochastic model updating strategy-based improved response surface model and advanced Monte Carlo simulation publication-title: Mech. Syst. Signal Process. – volume: 108 year: 2020 ident: br0080 article-title: Dynamic probabilistic-based LCF damage assessment of turbine blades regarding time-varying multi-physical field loads publication-title: Eng. Fail. Anal. – volume: 230 year: 2016 ident: br0020 article-title: Parametric modeling and updating for bolted joints of aeroengine casings publication-title: Proc. Inst. Mech. Eng., Part C, J. Mech. Eng. Sci. – volume: 26 start-page: 33 year: 2012 end-page: 42 ident: br0350 article-title: Advance first order second moment (AFOSM) method for single reservoir operation reliability analysis: a case study publication-title: Stoch. Environ. Res. Risk Assess. – volume: 30 year: 2016 ident: br0030 article-title: Reliability-based design optimization method of turbine disk with transformed deterministic constraints publication-title: J. Aerosp. Eng. – volume: 25 start-page: 365 year: 2010 end-page: 371 ident: br0210 article-title: An efficient response surface method using moving least squares approximation for structural reliability analysis publication-title: Probab. Eng. Mech. – volume: 54 start-page: 662 year: 2017 end-page: 671 ident: br0240 article-title: Multiobjective design optimization of hypersonic combinational novel cavity and opposing jet concept publication-title: J. Spacecr. Rockets – volume: 28 start-page: 297 year: 2013 end-page: 304 ident: br0260 article-title: Latin hypercube sampling applied to reliability-based multidisciplinary design optimization of a launch vehicle publication-title: Aerosp. Sci. Technol. – volume: 99 start-page: 77 year: 2016 end-page: 97 ident: br0270 article-title: Error estimates for the moving least-square approximation and the element-free Galerkin method in publication-title: Appl. Numer. Math. – volume: 282 start-page: 237 year: 2015 end-page: 250 ident: br0280 article-title: Analysis of moving least squares approximation revisited publication-title: J. Comput. Appl. Math. – volume: 10 start-page: 47 year: 2013 end-page: 52 ident: br0150 article-title: Extremum response surface method for casing radial deformation probabilistic analysis publication-title: J. Aerosp. Inform. Syst. – volume: 12 start-page: 1545 issue: 9 year: 2019 ident: 10.1016/j.ast.2020.106112_br0320 article-title: Reliability-based low fatigue life analysis of turbine blisk with generalized regression extreme neural network method publication-title: Materials doi: 10.3390/ma12091545 – volume: 155 start-page: 287 year: 2019 ident: 10.1016/j.ast.2020.106112_br0140 article-title: Design exploration of combinational spike and opposing jet concept in hypersonic flows based on CFD calculation and surrogate model publication-title: Acta Astronaut. doi: 10.1016/j.actaastro.2018.12.012 – volume: 86 start-page: 143 year: 2016 ident: 10.1016/j.ast.2020.106112_br0090 article-title: FEM-DBEM approach for crack propagation in a low pressure aeroengine turbine vane segment publication-title: Theor. Appl. Fract. Mech. doi: 10.1016/j.tafmec.2016.05.004 – volume: 34 start-page: 1225 issue: 5 year: 2010 ident: 10.1016/j.ast.2020.106112_br0310 article-title: Stochastic approach to kinematic reliability of open-loop mechanism with dimensional tolerance publication-title: Appl. Math. Model. doi: 10.1016/j.apm.2009.08.009 – volume: 39 start-page: 3914 year: 2014 ident: 10.1016/j.ast.2020.106112_br0100 article-title: Design exploration of three-dimensional transverse jet in a supersonic crossflow based on data mining and multi-objective design optimization approaches publication-title: Int. J. Hydrog. Energy doi: 10.1016/j.ijhydene.2013.12.129 – volume: 282 start-page: 237 year: 2015 ident: 10.1016/j.ast.2020.106112_br0280 article-title: Analysis of moving least squares approximation revisited publication-title: J. Comput. Appl. Math. doi: 10.1016/j.cam.2015.01.007 – volume: 46 start-page: 2459 issue: 10 year: 2008 ident: 10.1016/j.ast.2020.106112_br0290 article-title: Efficient global reliability analysis for nonlinear implicit performance functions publication-title: AIAA J. doi: 10.2514/1.34321 – volume: 33 start-page: 47 year: 2013 ident: 10.1016/j.ast.2020.106112_br0300 article-title: Metamodel-based importance sampling for structural reliability analysis publication-title: Probab. Eng. Mech. doi: 10.1016/j.probengmech.2013.02.002 – volume: 95 year: 2019 ident: 10.1016/j.ast.2020.106112_br0190 article-title: Decomposed-coordinated surrogate modelling strategy for compound function approximation and a turbine blisk reliability evaluation publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2019.105466 – volume: 21 start-page: 335 issue: 4 year: 2008 ident: 10.1016/j.ast.2020.106112_br0340 article-title: An efficient method for reliability-based multidisciplinary design optimization publication-title: Chin. J. Aeronaut. doi: 10.1016/S1000-9361(08)60044-8 – volume: 63 start-page: 603 issue: 2 year: 2014 ident: 10.1016/j.ast.2020.106112_br0120 article-title: Uncertainty quantification in remaining useful life prediction using first-order reliability methods publication-title: IEEE Trans. Reliab. doi: 10.1109/TR.2014.2313801 – volume: 37 start-page: 141 year: 1981 ident: 10.1016/j.ast.2020.106112_br0200 article-title: Surfaces generated by moving least squares methods publication-title: Math. Comput. doi: 10.1090/S0025-5718-1981-0616367-1 – volume: 266 start-page: 66 issue: C1 year: 2012 ident: 10.1016/j.ast.2020.106112_br0070 article-title: Efficient dynamic analysis of a whole aeroengine using identified nonlinear bearing models publication-title: Proc. Inst. Mech. Eng., Part C, J. Mech. Eng. Sci. doi: 10.1177/0954406211412319 – volume: 108 year: 2020 ident: 10.1016/j.ast.2020.106112_br0080 article-title: Dynamic probabilistic-based LCF damage assessment of turbine blades regarding time-varying multi-physical field loads publication-title: Eng. Fail. Anal. doi: 10.1016/j.engfailanal.2019.104193 – volume: 76 start-page: 164 year: 2018 ident: 10.1016/j.ast.2020.106112_br0170 article-title: Improved Kriging with extremum response surface method for structural dynamic reliability and sensitivity analyses publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2018.02.012 – volume: 25 start-page: 365 issue: 4 year: 2010 ident: 10.1016/j.ast.2020.106112_br0210 article-title: An efficient response surface method using moving least squares approximation for structural reliability analysis publication-title: Probab. Eng. Mech. doi: 10.1016/j.probengmech.2010.04.002 – volume: 82 start-page: 323 year: 2017 ident: 10.1016/j.ast.2020.106112_br0230 article-title: A stochastic model updating strategy-based improved response surface model and advanced Monte Carlo simulation publication-title: Mech. Syst. Signal Process. doi: 10.1016/j.ymssp.2016.05.026 – volume: 26 start-page: 33 issue: 1 year: 2012 ident: 10.1016/j.ast.2020.106112_br0350 article-title: Advance first order second moment (AFOSM) method for single reservoir operation reliability analysis: a case study publication-title: Stoch. Environ. Res. Risk Assess. doi: 10.1007/s00477-011-0517-1 – volume: 20 start-page: 302 issue: 2 year: 2004 ident: 10.1016/j.ast.2020.106112_br0010 article-title: Turbine engine clearance control systems: current practices and future directions publication-title: J. Propuls. Power doi: 10.2514/1.9255 – volume: 84 start-page: 641 year: 2019 ident: 10.1016/j.ast.2020.106112_br0050 article-title: Parametric modeling and aerodynamic optimization of EXPERT configuration at hypersonic speeds publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2018.11.007 – volume: 230 issue: 16 year: 2016 ident: 10.1016/j.ast.2020.106112_br0020 article-title: Parametric modeling and updating for bolted joints of aeroengine casings publication-title: Proc. Inst. Mech. Eng., Part C, J. Mech. Eng. Sci. doi: 10.1177/0954406215607900 – volume: 69 start-page: 440 issue: 2 year: 2020 ident: 10.1016/j.ast.2020.106112_br0380 article-title: Improved decomposed-coordinated Kriging modeling strategy for dynamic probabilistic analysis of multi-component structures publication-title: IEEE Trans. Reliab. doi: 10.1109/TR.2019.2954379 – volume: 64 start-page: 1517 issue: 224 year: 1998 ident: 10.1016/j.ast.2020.106112_br0250 article-title: The approximation power of moving least-squares publication-title: Math. Comput. doi: 10.1090/S0025-5718-98-00974-0 – volume: 48 start-page: 899 year: 2017 ident: 10.1016/j.ast.2020.106112_br0110 article-title: M5 model tree and Monte Carlo simulation for efficient structural reliability analysis publication-title: Appl. Math. Model. doi: 10.1016/j.apm.2017.02.047 – volume: 92 start-page: 464 year: 2019 ident: 10.1016/j.ast.2020.106112_br0180 article-title: Multi-failure probabilistic design for turbine bladed disks using neural network regression with distributed collaborative strategy publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2019.06.026 – volume: 60 start-page: 56 year: 2016 ident: 10.1016/j.ast.2020.106112_br0220 article-title: Reliability analysis of structures by iterative improved response surface method publication-title: Struct. Saf. doi: 10.1016/j.strusafe.2016.02.002 – volume: 55 start-page: 70 year: 2015 ident: 10.1016/j.ast.2020.106112_br0330 article-title: Reliability assessment of reinforced concrete columns based on the P-M interaction diagram using AFOSM publication-title: Struct. Saf. doi: 10.1016/j.strusafe.2015.03.003 – volume: 10 start-page: 47 issue: 1 year: 2013 ident: 10.1016/j.ast.2020.106112_br0150 article-title: Extremum response surface method for casing radial deformation probabilistic analysis publication-title: J. Aerosp. Inform. Syst. doi: 10.2514/1.I010045 – volume: 12 start-page: 2341 issue: 15 year: 2019 ident: 10.1016/j.ast.2020.106112_br0160 article-title: Fuzzy multi-SVR learning model for reliability-based design optimization of turbine blades publication-title: Materials doi: 10.3390/ma12152341 – volume: 54 start-page: 662 issue: 3 year: 2017 ident: 10.1016/j.ast.2020.106112_br0240 article-title: Multiobjective design optimization of hypersonic combinational novel cavity and opposing jet concept publication-title: J. Spacecr. Rockets doi: 10.2514/1.A33801 – volume: 137 issue: 3 year: 2015 ident: 10.1016/j.ast.2020.106112_br0060 article-title: Finite element modeling of shot peening residual stress relaxation in turbine disk assemblies publication-title: J. Eng. Mater. Technol. doi: 10.1115/1.4030066 – volume: 28 start-page: 297 issue: 1 year: 2013 ident: 10.1016/j.ast.2020.106112_br0260 article-title: Latin hypercube sampling applied to reliability-based multidisciplinary design optimization of a launch vehicle publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2012.11.010 – volume: 99 start-page: 77 year: 2016 ident: 10.1016/j.ast.2020.106112_br0270 article-title: Error estimates for the moving least-square approximation and the element-free Galerkin method in n-dimensional spaces publication-title: Appl. Numer. Math. doi: 10.1016/j.apnum.2015.07.006 – volume: 30 year: 2016 ident: 10.1016/j.ast.2020.106112_br0030 article-title: Reliability-based design optimization method of turbine disk with transformed deterministic constraints publication-title: J. Aerosp. Eng. – volume: 103 year: 2020 ident: 10.1016/j.ast.2020.106112_br0370 article-title: Multilevel nested reliability-based design optimization with hybrid intelligent regression for operating assembly relationship publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2020.105906 – volume: 100 year: 2020 ident: 10.1016/j.ast.2020.106112_br0040 article-title: Constraint-based parameterization using FFD and multi-objective design optimization of a hypersonic vehicle publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2020.105788 |
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| SubjectTerms | Dynamic reliability Fluid-thermal-structural interaction Importance sampling method Moving extremum surrogate modeling strategy Radial deformation Turbine blisk |
| Title | Moving extremum surrogate modeling strategy for dynamic reliability estimation of turbine blisk with multi-physics fields |
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