Citation: | Cui Kai, Yang Jing, Chang Siyuan, Tian Zhongwei, Xiao Yao, Li Guangli. Rapid prediction method for high-pressure capturing wing surface flow field based on proper orthogonal decomposition and surrogate model. Chinese Journal of Theoretical and Applied Mechanics, 2025, 57(4): 883-894. DOI: 10.6052/0459-1879-24-530 |
[1] |
蔡国飙, 徐大军. 高超声速飞行器技术. 北京: 科学出版社, 2012 (Cai Guobiao, Xu Dajun. Technology of Hypersonic Vehicle. Beijing: Science Press, 2012 (in Chinese)
Cai Guobiao, Xu Dajun. Technology of Hypersonic Vehicle. Beijing: Science Press, 2012 (in Chinese)
|
[2] |
Ding F, Liu J, Shen C, et al. An overview of research on waverider design methodology. Acta Astronautica, 2017, 140: 190-205 doi: 10.1016/j.actaastro.2017.08.027
|
[3] |
刘济民, 常斌, 张朝阳等. 乘波体特性研究现状及展望. 航空科学技术, 2023, 34(11): 23-33 (Liu Jimin, Chang Bin, Zhang Zhaoyang, et al. Research status and prospect on the charactaeristics of waverider. Aeronautical Science & Technology, 2023, 34(11): 23-33 (in Chinese)
Liu Jimin, Chang Bin, Zhang Zhaoyang, et al. Research status and prospect on the charactaeristics of waverider. Aeronautical Science & Technology, 2023, 34(11): 23-33 (in Chinese)
|
[4] |
唐伟, 冯毅, 杨肖峰等. 非惯性弹道飞行器气动布局设计实践. 气体物理, 2017, 2(1): 1-12 (Tang Wei, Feng Yi, Yang Xiaofeng, et al. Practices of aerodynamic configuration design for non-ballistic trajectory vehicles. Physics of Gases, 2017, 2(1): 1-12 (in Chinese)
Tang Wei, Feng Yi, Yang Xiaofeng, et al. Practices of aerodynamic configuration design for non-ballistic trajectory vehicles. Physics of Gases, 2017, 2(1): 1-12 (in Chinese)
|
[5] |
崔凯, 李广利, 肖尧等. 高速飞行器高压捕获翼气动布局概念研究. 中国科学: 物理学 力学 天文学, 2013, 43(5): 652-661 (Cui Kai, Li Guangli, Xiao Yao, et al. Conceptual studies of the high pressure zone capture wing configuration for high speed air vehicles. Scientia Sinica: Physica, Mechanica & Astronomica, 2013, 43(5): 652-661 (in Chinese)
Cui Kai, Li Guangli, Xiao Yao, et al. Conceptual studies of the high pressure zone capture wing configuration for high speed air vehicles. Scientia Sinica: Physica, Mechanica & Astronomica, 2013, 43(5): 652-661 (in Chinese)
|
[6] |
Cui K, Li GL, Xiao Y, et al. High-pressure capturing wing configurations. AIAA Journal, 2017, 55(6): 1909-1919 doi: 10.2514/1.J055395
|
[7] |
Li GL, Cui K, Xu YZ, et al. Experimental investigation of a hypersonic I-shaped configuration with a waverider compression surface. Science China Physics, Mechanics & Astronomy, 2020, 63(5): 25472
|
[8] |
Cui K, Xiao Y, Xu YZ, et al. Hypersonic I-shaped aerodynamic configurations. Science China Physics, Mechanics & Astronomy, 2018, 61(2): 024722
|
[9] |
Ma Y, Zhou W, Han QL, et al. Aerodynamic configuration of the HCW based on the lifting body. Journal of Aerospace Engineering, 2019, 32(2): 04019004 doi: 10.1061/(ASCE)AS.1943-5525.0000950
|
[10] |
Wang YL, Wei YJ, Wang C, et al. Theoretical and numerical simulation study on aerodynamics of V configuration high-pressure capture wing (HCW-V). Physics of Fluids, 2022, 34(8): 086106 doi: 10.1063/5.0102095
|
[11] |
常思源, 肖尧, 李广利等. 翼反角对高压捕获翼构型高超气动特性的影响. 航空学报, 2023, 44(8): 45-58 (Chang Siyuan, Xiao Yao, Li Guangli, et al. Effect of wing dihedral and anhedral angles on hypersonic aerodynamic characteristics of HCW configuration. Acta Aeronautica et Astronautica Sinica, 2023, 44(8): 45-58 (in Chinese)
Chang Siyuan, Xiao Yao, Li Guangli, et al. Effect of wing dihedral and anhedral angles on hypersonic aerodynamic characteristics of HCW configuration. Acta Aeronautica et Astronautica Sinica, 2023, 44(8): 45-58 (in Chinese)
|
[12] |
常思源, 田中伟, 李广利等. 基于气动导数的高压捕获翼飞行器纵向稳定性数值研究. 中国科学: 技术科学, 2024, 54(2): 275-288 (Chang Siyuan, Tian Zhongwei, Li Guangli, et al. Numerical study on longitudinal stability for HCW aircraft based on aerodynamic derivatives. Scientia Sinica: Technologica, 2024, 54(2): 275-288 (in Chinese) doi: 10.1360/SST-2022-0309
Chang Siyuan, Tian Zhongwei, Li Guangli, et al. Numerical study on longitudinal stability for HCW aircraft based on aerodynamic derivatives. Scientia Sinica: Technologica, 2024, 54(2): 275-288 (in Chinese) doi: 10.1360/SST-2022-0309
|
[13] |
肖尧, 崔凯, 李广利等. 高压捕获翼双翼构型宽速域气动性能研究. 气体物理, 2023, 8(5): 54-60 (Xiao Yao, Cui Kai, Li Guangli, et al. Research on aerodynamic performance of high-pressure capturing wing with bi-wing configuration in wide-speed range. Physics of Gases, 2023, 8(5): 54-60 (in Chinese)
Xiao Yao, Cui Kai, Li Guangli, et al. Research on aerodynamic performance of high-pressure capturing wing with bi-wing configuration in wide-speed range. Physics of Gases, 2023, 8(5): 54-60 (in Chinese)
|
[14] |
程锋, 唐硕, 张栋. 超声速/高超声速飞行器气动力快速估算平台设计及应用. 西北工业大学学报, 2018, 36(6): 1076-1084 (Cheng Feng, Tang Shuo, Zhang Dong. Design and applications of preliminary evaluation platform of aerodynamic forces for supersonic/hypersonic vehicles. Journal of Northwestern Polytechnical University, 2018, 36(6): 1076-1084 (in Chinese) doi: 10.3969/j.issn.1000-2758.2018.06.007
Cheng Feng, Tang Shuo, Zhang Dong. Design and applications of preliminary evaluation platform of aerodynamic forces for supersonic/hypersonic vehicles. Journal of Northwestern Polytechnical University, 2018, 36(6): 1076-1084 (in Chinese) doi: 10.3969/j.issn.1000-2758.2018.06.007
|
[15] |
郝佳傲, 蒋崇文, 高振勋等. 有翼再入飞行器的超/高超声速气动力工程方法. 中国空间科学技术, 2014, 34(3): 38-45 (Hao Jiaao, Jiang Chongwen, Gao Zhenxun, et al. Aerodynamic engineering prediction methods for winged reentry vehicles. Chinese Space Science and Technology, 2014, 34(3): 38-45 (in Chinese) doi: 10.3780/j.issn.1000-758X.2014.03.006
Hao Jiaao, Jiang Chongwen, Gao Zhenxun, et al. Aerodynamic engineering prediction methods for winged reentry vehicles. Chinese Space Science and Technology, 2014, 34(3): 38-45 (in Chinese) doi: 10.3780/j.issn.1000-758X.2014.03.006
|
[16] |
Lobbia MA. Rapid supersonic/hypersonic aerodynamics analysis model for arbitrary geometries. Journal of Spacecraft and Rockets, 2017, 54(1): 315-322 doi: 10.2514/1.A33514
|
[17] |
朱广生, 段毅, 姚世勇等. 跨流域高速飞行器气动设计研究现状及思考. 宇航学报, 2023, 44(3): 358-367 (Zhu Guangsheng, Duan Yi, Yao Shiyong, et al. Research status and consideration on aerodynamic design of hypersonic flight vehicle covering various flow regimes. Journal of Astronautics, 2023, 44(3): 358-367 (in Chinese)
Zhu Guangsheng, Duan Yi, Yao Shiyong, et al. Research status and consideration on aerodynamic design of hypersonic flight vehicle covering various flow regimes. Journal of Astronautics, 2023, 44(3): 358-367 (in Chinese)
|
[18] |
Andres-Perez E, Paulete-Perianez C. On the application of surrogate regression models for aerodynamic coefficient prediction. Complex & Inteligent Systems, 2021, 7(4): 1991-2021
|
[19] |
陈树生, 冯聪, 张兆康等. 基于全局/梯度优化方法的宽速域乘波-机翼布局气动设计. 航空学报, 2024, 45(6): 140-154 (Chen Shusheng, Feng Cong, Zhang Zhaokang, et al. Aerodynamic design of wide-speed-range waverider-wing configuration based on global & gradient optimization method. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 140-154 (in Chinese)
Chen Shusheng, Feng Cong, Zhang Zhaokang, et al. Aerodynamic design of wide-speed-range waverider-wing configuration based on global & gradient optimization method. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 140-154 (in Chinese)
|
[20] |
Jin SY, Chen SS, Che SQ, et al. Airfoil aerodynamic/stealth design based on conditional generative adversarial networks. Physics of Fluids, 2024, 36(7): 077146 doi: 10.1063/5.0220671
|
[21] |
Chen X, Wang Z, Deng L, et al. Towards a new paradigm in intelligence-driven computational fluid dynamics simulations. Engineering Applications of Computational Fluid Mechanics, 2024, 18(1): 2407005 doi: 10.1080/19942060.2024.2407005
|
[22] |
陈皓, 郭明明, 田野等. 卷积神经网络在流场重构研究中的进展. 力学学报, 2022, 54(9): 2343-2360 (Chen Hao, Guo Mingming, Tian Ye, et al. Progress of convolution neural networks in flow field reconstruction. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(9): 2343-2360 (in Chinese)
Chen Hao, Guo Mingming, Tian Ye, et al. Progress of convolution neural networks in flow field reconstruction. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(9): 2343-2360 (in Chinese)
|
[23] |
Long Y, Guo X, Xiao TB. Research, application and future prospect of mode decomposition in fluid mechanics. Symmetry, 2024, 16(2): 155 doi: 10.3390/sym16020155
|
[24] |
陈鑫, 刘莉, 岳振江. 基于本征正交分解和代理模型的高超声速气动热模型降阶研究. 航空学报, 2015, 36(2): 462-472 (Chen Xin, Liu Li, Yue Zhenjiang. Reduced order aerothermodynamic modeling research for hypersonic vehicles based on proper orthogonal decomposition and surrogate method. Acta Aeronautica et Astronautica Sinica, 2015, 36(2): 462-472 (in Chinese)
Chen Xin, Liu Li, Yue Zhenjiang. Reduced order aerothermodynamic modeling research for hypersonic vehicles based on proper orthogonal decomposition and surrogate method. Acta Aeronautica et Astronautica Sinica, 2015, 36(2): 462-472 (in Chinese)
|
[25] |
Dolci V, Arina R. Proper orthogonal decomposition as surrogate model for aerodynamic optimization. International Journal of Aerospace Engineering, 2016, 2016(1): 8092824
|
[26] |
赵啸宇. 融合先验知识的物理场快速预测深度代理模型方法研究. [博士论文]. 北京: 军事科学院, 2023 (Zhao Xiaoyu. Research on deep surrogate model method integrated with prior knowledge for fast prediction of physical fields. [PhD Thesis]. Beijing: Academy of Military Science, 2023 (in Chinese)
Zhao Xiaoyu. Research on deep surrogate model method integrated with prior knowledge for fast prediction of physical fields. [PhD Thesis]. Beijing: Academy of Military Science, 2023 (in Chinese)
|
[27] |
Crowell AR, McNamara JJ. Model reduction of computational aerothermodynamics for hypersonic aerothermoelasticity. AIAA Journal, 2012, 50(1): 74-84 doi: 10.2514/1.J051094
|
[28] |
Hall KC, Thomas JP, Dowell EH. Proper orthogonal decomposition technique for transonic unsteady aerodynamic flows. AIAA Journal, 2000, 38(10): 1853-1862 doi: 10.2514/2.867
|
[29] |
Simpson TW, Booker AJ, Ghosh D, et al. Approximation methods in multidisciplinary analysis and optimization: A panel discussion. Structural and Multidisciplinary Optimization, 2004, 27: 302-313
|
[30] |
何西旺, 杨亮亮, 冉仁杰等. 基于多评价标准的代理模型综合比较研究. 机械工程学报, 2022, 58(16): 403-419 (He Xiwang, Yang Liangliang, Ran Renjie, et al. Comparative studies of surrogate models based on multiple evaluation criteria. Journal of Mechanical Engineering, 2022, 58(16): 403-419 (in Chinese) doi: 10.3901/JME.2022.16.403
He Xiwang, Yang Liangliang, Ran Renjie, et al. Comparative studies of surrogate models based on multiple evaluation criteria. Journal of Mechanical Engineering, 2022, 58(16): 403-419 (in Chinese) doi: 10.3901/JME.2022.16.403
|
[31] |
Xi XZ, Li GL, Zhang KK, et al. Surrogate-based shape optimization and sensitivity analysis on the aerodynamic performance of HCW configuration. Aerospace Science and Technology, 2024, 152: 109347 doi: 10.1016/j.ast.2024.109347
|
[32] |
方开泰, 刘民千, 周永道. 试验设计与建模. 北京: 高等教育出版社, 2011 (Fang Kaitai, Liu Minqian, Zhou Yongdao. Design and Modeling of Experiments. Beijing: Higher Education Press, 2011 (in Chinese)
Fang Kaitai, Liu Minqian, Zhou Yongdao. Design and Modeling of Experiments. Beijing: Higher Education Press, 2011 (in Chinese)
|
[33] |
Wong TT. Performance evaluation of classification algorithms by k-fold and leave-one-out cross validation. Pattern Recognition, 2015, 48(9): 2839-2846 doi: 10.1016/j.patcog.2015.03.009
|
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