Prediction of ice shape characteristic parameters based on BP nerual network
-
摘要: 机翼结冰影响了飞机飞行的气动特性,严重时将会引起事故,对冰形特征参数进行预测对翼型气动特性研究以及后续防除冰措施具有重要的意义。本文利用BP神经网络,建立翼型冰形特征参数预测模型,并采用k折交叉验证进行网络结构选择,以气象与飞行条件作为输入,结冰极限、冰角高度和角度等冰形特征参数作为输出。结果表明:预测的冰形特征参数(除下冰角高度外)与数值结果相对误差低于5%,证明该方法具有较好的预测效果。Abstract: Airfoil icing affects the aerodynamic characteristics of aircraft flight, which can lead to accidents when it is serious. The prediction of ice shape parameters can effectively prevent accidents. In this paper, BP neural network is used to establish the prediction model of airfoil ice shape characteristic parameters, and k-fold cross validation is used to select the network structure, in which the meteorological and flight conditions are the inputs, and ice shape characteristic parameters such as the ice limit, the ice angle height and angle are the outputs. The experimental results show that the relative error between the predicted ice shape parameters (except for the height of the lower ice angle) and the numerical results is less than 5%, which proves that the method has a good prediction ability.
-
表 1 气象和飞行条件参数设置
Table 1. Meteorological and flight condition parameters setting
参数 设置范围 飞行速度v/(m·s-1) 70~150 环境温度T/K 243~267 液态水含量LWC/(g·m-3) 0.2~0.8 平均水滴直径MVD/μm 20~60 结冰时间t/s 360~1350 表 2 算例的气象和飞行条件参数
Table 2. Meteorological and flight parameters of cases
算例 v/(m·s-1) T/K LWC/(g·m-3) MVD/μm t/s 1 85 243 0.75 40 420 2 90 243 0.75 20 300 3 67 245 0.6 15 540 4 77 258 0.8 30 600 5 110 263 0.85 40 540 6 77 260 0.6 30 540 7 88 245 0.9 33 480 8 92 255 0.6 25 480 表 3 冰形特征参数计算与预测结果
Table 3. Calculation and prediction results of ice shape characteristic parameters
算例 Su/(m·c-1) Sl/(m·c-1) hu/(m·c-1) hl/(m·c-1) θu/(°) θl/(°) 1 C 0.0490 -0.1444 0.0213 0.0207 183.5 225.0 P 0.0489 -0.1472 0.0211 0.0220 186.8 225.5 2 C 0.0278 -0.0623 0.0147 0.0143 209.3 231.6 P 0.0269 -0.0631 0.0137 0.0120 212.8 229.3 3 C 0.0212 -0.0366 0.0116 0.0111 212.9 237.0 P 0.0228 -0.0349 0.0111 0.0118 215.0 230.4 4 C 0.0381 -0.1022 0.0363 0.0245 177.0 267.7 P 0.0357 -0.1021 0.0354 0.0317 176.5 265.4 5 C 0.0522 -0.1624 0.0365 0.0160 127.3 288.5 P 0.0481 -0.1760 0.0366 0.0178 129.0 284.1 6 C 0.0358 -0.1022 0.0242 0.0179 183.3 270.4 P 0.0368 -0.1002 0.0228 0.0251 185.6 270.9 7 C 0.0432 -0.1184 0.0298 0.0280 202.1 236.6 P 0.0401 -0.1251 0.0286 0.0353 194.8 226.8 8 C 0.0261 -0.0572 0.0163 0.0151 208.0 230.6 P 0.0255 -0.0557 0.0160 0.0167 206.5 232.0 表 4 冰形特征参数预测误差
Table 4. Prediction error of ice shape characteristic parameters
算例 Su/(m·c-1) Sl/(m·c-1) hu/(m·c-1) hl/(m·c-1) θu/(°) θl/(°) APE/% 1 0.20 1.94 0.94 6.28 1.79 0.22 2 3.23 1.28 6.80 16.08 1.67 0.99 3 7.55 4.64 4.31 6.31 0.99 2.78 4 6.30 0.10 2.48 29.39 0.29 0.87 5 7.85 8.37 0.27 11.25 1.33 1.54 6 2.79 1.96 5.79 40.22 1.23 0.19 7 7.18 5.66 4.03 26.07 3.64 4.14 8 2.30 2.62 1.84 10.60 0.72 0.61 MAPE/% 4.68 3.32 3.31 18.28 1.46 1.42 -
[1] CEBECI T, KAFYEKE F. Aircrafticing[J]. Annual Review of Fluid Mechanics, 2003, 35(1): 11-21. doi: 10.1146/annurev.fluid.35.101101.161217 [2] 王建涛, 易贤, 肖中云, 等. ARJ21-700飞机冰脱落数值模拟[J]. 空气动力学学报, 2013, 31(4): 430-436. https://www.cnki.com.cn/Article/CJFDTOTAL-KQDX201304004.htmWANG J T, YI X, XIAO Z Y, et al. Numerical simulation of ice shedding from ARJ21-700[J]. Acta Aerodynamica Sinica, 2013, 31(4): 430-436. https://www.cnki.com.cn/Article/CJFDTOTAL-KQDX201304004.htm [3] RATVASKY T P, BARNHART B P, LEE S. Current methods modeling and simulating icing effects on aircraft performance, stability, control[J]. Journal of Aircraft, 2010, 47(1): 201-211. doi: 10.2514/1.44650 [4] 闫鹏庆, 牛亚宏. 人工模拟结冰飞行试验技术研究[J]. 民用飞机设计与研究, 2018(1): 71-74. doi: 10.19416/j.cnki.1674-9804.2018.01.013YAN P Q, NIU Y H. Research on artificial icing flight test technology[J]. Civil Aircraft Design & Research, 2018(1): 71-74. doi: 10.19416/j.cnki.1674-9804.2018.01.013 [5] 高郭池, 丁丽, 李保良, 等. 气动除冰类飞机结冰风洞试验适航审定技术[J]. 实验流体力学, 2019, 33(2): 85-94. doi: 10.11729/syltlx20180067GAO G C, DING L, LI B L, et al. Airworthiness certification technology about icing wind tunnel test for pneumatic de-icing aircraft[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(2): 85-94. doi: 10.11729/syltlx20180067 [6] 李鑫, 白俊强, 王昆. 机翼积冰数值模拟[J]. 航空动力学报, 2013, 28(12): 2663-2670. doi: 10.13224/j.cnki.jasp.2013.12.005LI X, BAI J Q, WANG K. Numerical simulation of ice accretions on aircraft wing[J]. Journal of Aerospace Power, 2013, 28(12): 2663-2670. doi: 10.13224/j.cnki.jasp.2013.12.005 [7] 张强, 陈迎春, 周涛, 等. 民用飞机机翼结冰试验与数值预测[J]. 航空动力学报, 2017, 32(1): 22-26. doi: 10.13224/j.cnki.jasp.2017.01.004ZHANG Q, CHEN Y C, ZHOU T, et al. Test and numerical prediction of ice accretions on civil aircraft wing[J]. Journal of Aerospace Power, 2017, 32(1): 22-26. doi: 10.13224/j.cnki.jasp.2017.01.004 [8] SAE. ARP5904, Airborne Icing Tankers[S]. Washington: Society of Automotive Engineers, 2007. [9] FOSSATI M, HABASHI W G. Multiparameter analysis of aero-icing problems using proper orthogonal decomposition and multidimensional interpolation[J]. AIAA Journal, 2013, 51(4): 946-960. doi: 10.2514/1.J051877 [10] OGRETIM E, HUEBSCH W, SHINN A. Aircraft ice accretion prediction based on neural networks[J]. Journal of Aircraft, 2006, 43(1): 233-240. doi: 10.2514/1.16241 [11] 潘环, 艾剑良. 飞机结冰冰形预测的建模与仿真[J]. 系统仿真学报, 2014, 26(1): 221-224, 229. doi: 10.16182/j.cnki.joss.2014.01.009PAN H, AI J L. Modeling and simulation of aircraft ice shape prediction[J]. Journal of System Simulation, 2014, 26(1): 221-224, 229. doi: 10.16182/j.cnki.joss.2014.01.009 [12] CHANG S N, LENG M Y, WU H W, et al. Aircraft ice accretion prediction using neural network and wavelet packet transform[J]. Aircraft Engineering and Aerospace Technology, 2016, 88(1): 128-136. doi: 10.1108/aeat-05-2014-0057 [13] 张强, 高正红. 基于神经网络的翼型积冰预测[J]. 飞行力学, 2011, 29(2): 6-9. doi: 10.13645/j.cnki.f.d.2011.02.002ZHANG Q, GAO Z H. Prediction of ice accretions based on the neural net[J]. Flight Dynamics, 2011, 29(2): 6-9. doi: 10.13645/j.cnki.f.d.2011.02.002 [14] KIM H, BRAGG M. Effects of leading-edge ice accretion geometry on airfoil performance[C]//Proc of the 17th Applied Aerodynamics Conference. 1999. doi: 10.2514/6.1999-3150 [15] BRAGG M, BROEREN A, ADDY H, et al. Airfoil ice-accretion aerodynamic simulation[R]. AIAA-2007-0085, 2007. doi: 10.2514/6.2007-85 [16] RUFF G, ANDERSON D. Quantification of ice accretions for icing scaling evaluations[R]. AIAA-98-0915, 1998. doi: 10.2514/6.1998-195 [17] SAE. AIR5666, Icing wind tunnel interfacility comparison tests[S]. Washington: SAE Aero-space Information Report, 2012. [18] 易贤. 飞机积冰的数值计算与积冰试验相似准则研究[D]. 绵阳: 中国空气动力研究与发展中心, 2007.YI X. Numerical computation of aircraft icing and study on icing test scaling law[D]. Mianyang: China Aerodynamics Research and Development Center, 2007. [19] 王小川, 史峰, 郁磊. MATLAB神经网络43个案例分析[M]. 北京: 北京航空航天大学出版社, 2013.WANG X C, SHI F, YU L. Analysis of 43 cases of MATLAB neural network[M]. Beijing: Beijing University of Aeronautics & Astronautics Press, 2013.