Citation: | XIAO Zhipeng, QIAN Wenmin, ZHOU Leiet al. Aeroelastic optimization design of composite wing for large aircraft with panel stiffness matching[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(8): 1629-1635. doi: 10.13700/j.bh.1001-5965.2017.0613(in Chinese) |
A method of aeroelastic optimization design with consideration of panel stiffness matching was developed for the composite wing of large aircraft. The optimization was performed based on the sensitivity algorithm, and the objective was to minimize the structural mass subject to the constraints of panel stiffness matching, flutter speed, deformation at wingtip, design allowable and manufacturability. The composite wings were designed in the case of critical load conditions. The influences of various panel stiffness matching requirements on optimal design results were studied and they were compared with the conventional optimal design results. The results indicate that the structural weight will increase with consideration of panel stiffness matching. However, it has an advantage in local buckling design, damage tolerance design and manufacturing of large composite panel. The optimal design results can be significantly affected by the design ranges of panel stiffness matching, so these design ranges should be properly determined according to the requirements of design and manufacturing. The design allowable of compression is a crucial constraint of the aeroelastic optimization design for composite wing.
[1] |
杜善义.先进复合材料与航空航天[J].复合材料学报, 2007, 24(1):1-12. doi: 10.3321/j.issn:1000-3851.2007.01.001
DU S Y.Advanced composite materials and aerospace engineering[J].Acta Materiae Compositae Sinica, 2007, 24(1):1-12(in Chinese). doi: 10.3321/j.issn:1000-3851.2007.01.001
|
[2] |
ZHANG X, LI Y.Damage tolerance and fail safety of welded aircraft wing panels[J].AIAA Journal, 2012, 43(7):1613-1623.
|
[3] |
ROUSE M, AMBUR D R.Damage tolerance and failure analysis of a composite geodesically stiffened compression panel[J].Journal of Aircraft, 2015, 33(3):582-588. doi: 10.2514/3.46985
|
[4] |
CHRISTOS C C, MINNETYAN L.Defect/damage tolerance of pressurized fiber composite shells[J].Composite Structures, 2001, 51(2):159-168. doi: 10.1016/S0263-8223(00)00141-0
|
[5] |
GURDAL Z, TATTING B F, WU C K.Variable stiffness composite panels:Effects of stiffness variation on the in-plane and buckling response[J].Composites Part A, 2008, 39(5):911-922. doi: 10.1016/j.compositesa.2007.11.015
|
[6] |
赵群, 丁运亮, 金海波.基于压弯刚度匹配论则的复合材料加筋板结构优化设计[J].南京航空航天大学学报, 2010, 42(3):357-362. doi: 10.3969/j.issn.1005-2615.2010.03.020
ZHAO Q, DING Y L, JIN H B.Structural optimization design of composite stiffened panels based on matching regulations of compression and bending stiffnesses[J].Journal of Nanjing University of Aeronautics & Astronautics, 2010, 42(3):357-362(in Chinese). doi: 10.3969/j.issn.1005-2615.2010.03.020
|
[7] |
乔巍, 姚卫星.复合材料加筋板铺层优化设计的等效弯曲刚度法[J].计算力学学报, 2011, 28(1):158-162.
QIAO W, YAO W X.Equivalent bending stiffness method for stacking sequence optimization of composite stiffed panel[J].Chinese Journal of Computational Mechanics, 2011, 28(1):158-162(in Chinese).
|
[8] |
TERRENCE A W, DAVID K D.Induced drag reduction using aeroelastic tailoring with adaptive control surfaces[J].Journal of Aircraft, 2006, 43(1):157-164. doi: 10.2514/1.12040
|
[9] |
GUO S J, CHENG W Y, CUI D G.Aeroelastic tailoring of composite wing structures by laminate layup optimization[J].AIAA Journal, 2006, 44(12):3146-3149. doi: 10.2514/1.20166
|
[10] |
LIANG L, WAN Z Q, YANG C.Aeroelastic optimization on composite skins of large aircraft wings[J].Science China Technological Sciences, 2012, 55(4):1078-1085. doi: 10.1007/s11431-011-4734-0
|
[11] |
DILLINGER J K S, KLIMMEK T, ABDALLA M M, et al.Stiffness optimization of composite wings with aeroelastic constraints[J].Journal of Aircraft, 2013, 50(4):1159-1168. doi: 10.2514/1.C032084
|
[12] |
周磊, 万志强, 杨超.复合材料壁板铺层参数对大展弦比机翼气动弹性优化的影响[J].复合材料学报, 2013, 30(5):195-200. doi: 10.3969/j.issn.1000-3851.2013.05.030
ZHOU L, WAN Z Q, YANG C.Effect of laminate parameter of composite skin on aeroelastic optimization of high-aspect-wing[J].Acta Materiae Compositae Sinica, 2013, 30(5):195-200(in Chinese). doi: 10.3969/j.issn.1000-3851.2013.05.030
|
[13] |
万志强, 杨超.大展弦比复合材料机翼气动弹性优化[J].复合材料学报, 2005, 22(3):145-149. doi: 10.3321/j.issn:1000-3851.2005.03.028
WAN Z Q, YANG C.Aeroelastic optimization of a high-aspect-ratio composite wing[J].Acta Materiae Compositae Sinica, 2005, 22(3):145-149(in Chinese). doi: 10.3321/j.issn:1000-3851.2005.03.028
|
[14] |
RODDEN W P, JOHNSON E H.MSC/Nastran aeroelastic ana-lysis user's guide V68[M].Los Angeles, CA:MSC.Software Corporation, 1994:657-698.
|
[15] |
万志强, 杨超.设计敏度在气动弹性遗传优化中的应用[J].北京航空航天大学学报, 2006, 32(5):508-512. doi: 10.3969/j.issn.1001-5965.2006.05.003
WAN Z Q, YANG C.Application of design sensitivity in aeroelastic genetic optimization[J].Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(5):508-512(in Chinese). doi: 10.3969/j.issn.1001-5965.2006.05.003
|
[16] |
林梦鹤, 孙宪学.气动弹性剪裁中的响应值敏度[J].航空学报, 2001, 22(1):30-34. doi: 10.3321/j.issn:1000-6893.2001.01.007
LIN M H, SUN X X.Response sensitivity in aeroelastic tailoring[J].Acta Aeronautica et Astronautica Sinica, 2001, 22(1):30-34(in Chinese). doi: 10.3321/j.issn:1000-6893.2001.01.007
|
[17] |
中国航空研究院.复合材料结构稳定性分析指南[M].北京:航空工业出版社, 2002:137-141.
Chinese Institute of Aeronautics.Analysis guide for composite structural stability[M].Beijing:Aviation Industry Press, 2002:137-141(in Chinese).
|
[18] |
霍世慧, 王富生, 王佩艳, 等.复合材料机翼加筋壁板稳定性分析[J].应用力学学报, 2010, 27(2):423-427.
HUO S H, WANG F S, WANG P Y, et al.Stability analysis on the ribbed panel of the composite wing[J].Chinese Journal of Applied Mechanics, 2010, 27(2):423-427(in Chinese).
|
[19] |
金迪, 寇艳荣.复合材料加筋壁板结构选型设计[J].复合材料学报, 2016, 33(5):1142-1146.
JIN D, KOU Y R.Structural style-selection design of composite stiffened panel[J].Acta Materiae Compositae Sinica, 2016, 33(5):1142-1146(in Chinese).
|
[1] | FU Yangaoxiao, MEI Jie, DING Mingsong, CHEN Jianqiang, JIANG Tao, DONG Weizhong. Numerical simulation of jet interaction heating on reusable launch vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2025.0053 |
[2] | ZHANG Yu, WANG Fengming, WANG Yanhong, MU Lin, DONG Ming. Simulation of combustion characteristics and prediction of combustion performance using machine learning in an integrated afterburner[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0213 |
[3] | SU Jinxin, XI Ziyan, DAI Yuting. Nonlinear fluid-structure interaction response analysis of a large flexible wing under strong gusts[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0278 |
[4] | BAI Jianfeng, MENG Junhui, ZHANG Lili, WEI Shechun, MA Nuo. Dynamic performances research of the wing deployment considering fluid structure interaction[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0645 |
[5] | ZOU L,WU W N,LIU J,et al. Numerical simulation of flow around two tandem wavy conical cylinders at subcritical Reynolds number[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(3):706-715 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0285. |
[6] | LI M J,GUO Z H. Combustion instability analysis of pilot flame in model combustor[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(3):951-961 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0274. |
[7] | HE Yan-tong, DENG Tian. Numerical Study of low-pressure modeling of bio-jet fuel combustion[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0826 |
[8] | LI C Q,ZHAN Y Q,WANG Z M,et al. Numerical simulation of iliac vein compression syndrome in hemodynamics[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(8):2646-2654 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0693. |
[9] | LEI J M,WU Z X,XIE W Y. Numerical simulation investigation on water surface skipping motion characteristics of sea-skimming projectile[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(10):2975-2983 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0813. |
[10] | CHEN B,LUO L,JIANG A L,et al. Numerical simulation of separation characteristics for internally buried weapon at high Mach number[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(7):2113-2122 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0627. |
[11] | ZHANG Pei-hong, JIA Hong-yin, ZHAO Jiao, WU Xiao-jun, ZHOU Gui-yu, ZHANG Yao-bing. Numerical simulation research on opposing jet interaction characteristics of rocket inverse flight[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0710 |
[12] | ZHANG P H,CHEN H Y,ZHANG J,et al. Passive flow control for weapon bay at high Mach number[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(11):2913-2920 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0790. |
[13] | XIE N,TANG Y M,ZHANG Y,et al. Numerical study of blood pump weaning effects on hemocompatibility of centrifugal blood pump[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(7):1680-1688 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0494. |
[14] | ZHANG P H,TANG Y,TANG J,et al. Simulation of cavity flow at high Mach number based on adaptive unstructured hybrid mesh[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(6):1311-1318 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0424. |
[15] | HAN Y F,HU X S,GAO Y,et al. Comparison of turbulence models for unsteady flow simulation in a long and narrow cabin[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(4):957-964 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0335. |
[16] | PENG L,LI L,ZHAO W. Numerical study on coupled heat transfer of rotating disc in centrifugal atomization[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(12):3456-3466 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0152. |
[17] | GUO Qi, SHEN Xiaobin, LIN Guiping, ZHANG Shijuan. Numerical simulation of icing on aircraft rotating surfaces[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2259-2269. doi: 10.13700/j.bh.1001-5965.2021.0081 |
[18] | LI Yongchang, DAI Yuting, YANG Chao. Fluid and structure coupling analysis of split drag rudder[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2494-2501. doi: 10.13700/j.bh.1001-5965.2021.0151 |
[19] | WANG Tao, ZHANG Wanxin, LI Meng, BU Xueqin, ZHANG Chen, WANG Hailiang. Performance analysis of skin temperature prediction model combining Smith's thermoregulation model with Tanabe model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2482-2493. doi: 10.13700/j.bh.1001-5965.2021.0143 |
[20] | WENG Huiyan, CAI Guobiao, ZHENG Hongru, LIU Lihui, ZHANG Baiyi, HE Bijiao. Numerical simulation of effect of background pressure on electric propulsion plume field[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1854-1862. doi: 10.13700/j.bh.1001-5965.2021.0039 |