The Aero-Engine Component-Level Modelling Research Based on NSDE Hybrid Damping Newton Method
Advanced aero-engine component-level models are characterized by strong nonlinearity and multivariate, and traditional iterative algorithms cannot meet the requirements of convergence, real-time, and accuracy at the same time. To improve the convergence and alleviate the initial value dependence, a...
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| Format: | Article |
| Language: | English |
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Wiley
2022-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2022/8212150 |
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| author | Chen Wang Ximing Sun Xian Du |
| author_facet | Chen Wang Ximing Sun Xian Du |
| author_sort | Chen Wang |
| collection | DOAJ |
| description | Advanced aero-engine component-level models are characterized by strong nonlinearity and multivariate, and traditional iterative algorithms cannot meet the requirements of convergence, real-time, and accuracy at the same time. To improve the convergence and alleviate the initial value dependence, a hybrid damped Newton algorithm based on the neighborhood based speciation differential evolution (NSDE) is proposed in this paper for solving the aero-engine component-level model. The computational efficiency and convergence of the hybrid damped Newton algorithm and NSDE hybrid damped Newton algorithm under four typical steady-state operating point conditions are analyzed, and then, the accuracy of the model is verified. It is demonstrated that the hybrid damped Newton method has the advantage of low initial value sensitivity and high computational efficiency under large deviation conditions. The hybrid damped Newton method is more efficient than the Broyden algorithm in terms of iterative efficiency, faster than the traditional N-R algorithm in terms of computation speed, and has the highest computational convergence rate under the four typical operating conditions, but it cannot eliminate the initial value dependence. The NSDE hybrid damped Newton method offers high simulation accuracy and greatly increases computational real-time performance under large deviation conditions, and the maximum error between the numerical simulation results and the experimental reference value is 8.1%. This study provides advanced theoretical support for component-level modelling and has certain engineering application value. |
| format | Article |
| id | doaj-art-ab7f24748701415e882f3f8ac4c0b1f0 |
| institution | Kabale University |
| issn | 1687-5974 |
| language | English |
| publishDate | 2022-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-ab7f24748701415e882f3f8ac4c0b1f02025-08-20T03:39:40ZengWileyInternational Journal of Aerospace Engineering1687-59742022-01-01202210.1155/2022/8212150The Aero-Engine Component-Level Modelling Research Based on NSDE Hybrid Damping Newton MethodChen Wang0Ximing Sun1Xian Du2Dalian University of TechnologyDalian University of TechnologyDalian University of TechnologyAdvanced aero-engine component-level models are characterized by strong nonlinearity and multivariate, and traditional iterative algorithms cannot meet the requirements of convergence, real-time, and accuracy at the same time. To improve the convergence and alleviate the initial value dependence, a hybrid damped Newton algorithm based on the neighborhood based speciation differential evolution (NSDE) is proposed in this paper for solving the aero-engine component-level model. The computational efficiency and convergence of the hybrid damped Newton algorithm and NSDE hybrid damped Newton algorithm under four typical steady-state operating point conditions are analyzed, and then, the accuracy of the model is verified. It is demonstrated that the hybrid damped Newton method has the advantage of low initial value sensitivity and high computational efficiency under large deviation conditions. The hybrid damped Newton method is more efficient than the Broyden algorithm in terms of iterative efficiency, faster than the traditional N-R algorithm in terms of computation speed, and has the highest computational convergence rate under the four typical operating conditions, but it cannot eliminate the initial value dependence. The NSDE hybrid damped Newton method offers high simulation accuracy and greatly increases computational real-time performance under large deviation conditions, and the maximum error between the numerical simulation results and the experimental reference value is 8.1%. This study provides advanced theoretical support for component-level modelling and has certain engineering application value.http://dx.doi.org/10.1155/2022/8212150 |
| spellingShingle | Chen Wang Ximing Sun Xian Du The Aero-Engine Component-Level Modelling Research Based on NSDE Hybrid Damping Newton Method International Journal of Aerospace Engineering |
| title | The Aero-Engine Component-Level Modelling Research Based on NSDE Hybrid Damping Newton Method |
| title_full | The Aero-Engine Component-Level Modelling Research Based on NSDE Hybrid Damping Newton Method |
| title_fullStr | The Aero-Engine Component-Level Modelling Research Based on NSDE Hybrid Damping Newton Method |
| title_full_unstemmed | The Aero-Engine Component-Level Modelling Research Based on NSDE Hybrid Damping Newton Method |
| title_short | The Aero-Engine Component-Level Modelling Research Based on NSDE Hybrid Damping Newton Method |
| title_sort | aero engine component level modelling research based on nsde hybrid damping newton method |
| url | http://dx.doi.org/10.1155/2022/8212150 |
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