某夹芯结构抗鸟撞分析与设计

doi:CNKI:11-1929/V.20111031.1056.001

Abstract

Abstract: This paper provides a new design of a sandwich structure used in aircafts. To optimize this design, bird-strike tests are carried out on a sandwich structure made of a honeycomb core and aluminum cover plates, and a numerical model of this structure is developed with the explicit finite element program PAM-CRASH. The results of simulation, which describes the failure of the sandwich structure, agree well with test results. An improved structure is developed based on this result and bird-strike tests are carried out on the new structure. The reliability of the design is proved and the improved structure shows good behavior against bird-strikes in the tests.

Key words: bird-strike, PAM-CRASH, bird-strike test, numerical simulation, honeycomb-based sandwich

CLC Number:

V214.6

SHI Xiaopeng, LI Yulong, LIU Jun, WANG Yi, WANG Bing, CHEN Lufeng, SUN Weiwei. Analysis and Design for a Bird-strike Resistance Sandwich Structure[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(1): 68-76.

References

[1] Dolbeer R A,Wright S E,Weller J,et al.Wildlife strike to civil aircraft in the United States 1990-2008.FAA National Wildlife Strike Database Serial Report No.15.Washington:FAA,2009.

[2] Kuckuck H.Bird strike test with radomes and windscreens of the HFB 320 Hansa jet and Transall C160. Bird Strike Committee Europe (BSCE),13th Meeting.1978.

[3] Boroughs R.High speed bird impact analysis of the Learjet 45 windshield using DYNA3D.AIAA-1998-1705, 1998.

[4] Airoldi A,Tagliapietra D.Bird impact simulation against a hybrid composite and metallic vertical stabilizer.AIAA-2001-1390, 2001.

[5] Kermanidis T H,Labeas G,Sunaric M,et al.Development and validation of a novel bird strike resistant composite leading edge structure.Applied Composite Materials 2005,12(6): 327-353.

[6] McCarthy M A,Xiao J R,Petrinic N,et al.Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates—Part 1:material modelling. Applied Composite Materials, 2004, 11(5): 295-315.

[7] McCarthy M A,Xiao J R,Petrinic N,et al.Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates—Part 2:modelling of impact with SPH bird model.Applied Composite Materials,2004, 11(5): 317-340.

[8] Guida M,Marulo F,Meo M,et al.SPH—Lagrangian study of bird impact on leading edge wing.Composite Structures, 2011, 93(3): 1060-1071.

[9] Zhang Y K,Li Y L.Analysis of the bird impact resistance of different beam-edge structures.Mechanical Science and Technology for Aerospace Engineering, 2007, 26(12): 1595-1599.(in Chinese) 张永康, 李玉龙. 不同构型梁-缘结构抗鸟撞性能分析. 机械科学与技术, 2007, 26(12): 1595-1599.

[10] Zhang Y K, Li Y L, Wang H Q. Finite element analysis of bird impact damage to representative beam-edge structure. Explosion and Shock Waves, 2008, 28(3): 236-242.(in Chinese) 张永康, 李玉龙, 汪海青. 典型梁-缘结构鸟撞破坏的有限元分析. 爆炸与冲击, 2008, 28(3): 236-242.

[11] Wu L, Guo Y N, Li Y L. Bird strike simulation on sandwich composite structure of aircraft radome. Explosion and Shock Waves, 2009, 29(6): 642-647.(in Chinese) 毋玲, 郭英男, 李玉龙. 蜂窝夹芯雷达罩结构的鸟撞数值分析. 爆炸与冲击, 2009, 29(6): 642-647.

[12] Hanssen A G, Girardet Y, Olovsson L, et al. Numerical model for bird strike of aluminium foam-based sandwich panels. International Journal of Impact Engineering, 2006, 32(7): 1127-1144.

[13] Wilbeck J S, Barber J P. Bird impact loading. The Shock and Vibration Bulletin, 1978, 48(2): 115-122.

[14] Goyal V K, Huertas C A, Borrero J R, et al. Robust bird-strike modeling based on ALE formulation using LS-DYNA. AIAA-2006-1759, 2006.

[15] Goyal V, Huertas C A, Borrero J R, et al. Robust bird-strike modeling based on SPH formulation using LS-DYNA. AIAA-2006-1878, 2006.

Analysis and Design for a Bird-strike Resistance Sandwich Structure

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Chang WANG, Long HE, Dongxia XU, Min TANG, Shuai MA, Ximing WU. Flow control drag reduction of hub on coaxial rigid rotor aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529084-529084.
[2]	Jiang LAI, Zhaolin FAN, Qian WANG, Siwei DONG, Fulin TONG, Xianxu YUAN. Direct numerical simulation of hypersonic cone-flare model at angle of attack [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128610-128610.
[3]	Hongjian ZHANG, Yanxin ZHANG, Jianjun XIONG, Zhao ZHAO, Lin RAN, Xian YI. Numerical simulation of phased array ultrasonic beam propagation characteristics in ice layer [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729289-729289.
[4]	Yalu FU, Xianxu YUAN, Pengxin LIU, Ming YU. Statistical properties of thermodynamic fluctuations in compressible wall⁃bounded turbulence [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(9): 127217-127217.
[5]	Rong HAN, Wei LIU, Xiaoliang YANG. Dynamic drag reduction mechanism of self-aligned aerodisks on hypersonic aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(4): 126633-126633.
[6]	Pinpeng ZENG, Shusheng CHEN, Jinping LI, Muliang JIA, Zhenghong GAO. Numerical simulation of heat reduction on blunt-headed bodies by combined scheme of drag reduction spike and annular jets [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(22): 128407-128407.
[7]	Fenfen XIONG, Zexian LI, Yu LIU, Tangfan XIAHOU. A review of characterization methods for parameter uncertainty in engineering design based on numerical simulation [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(22): 28611-028611.
[8]	Yunlong ZHENG, Peiqing LIU, Qiulin QU, Jiahua DAI, Yu TIAN. Numerical investigation on motion characteristics of BWB aircraft in ditching [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(21): 528588-528588.
[9]	Xia HUANG, Fan LIU, Zhitao LIU, Jinhua WU. Correlation between numerical simulation and wind tunnel test results of soft refueling [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(20): 628447-628447.
[10]	Yang ZHANG, Jiaqi LUO, Xian ZENG. Elliptic flow noise by improved ghost⁃cell immersed boundary method [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(19): 128418-128418.
[11]	Yijian MA, Delin CHAI, Xian YI, Jingguo QU, Qiang WANG. Calculation method for ice crystal/mixed phase icing considering ice crystal erosion [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 528609-528609.
[12]	Junyang LI, Pengxin LIU, Ming YU, Dong SUN, Siwei DONG, Xianxu YUAN. Effects of viscous dissipation on wall heat flux in high-enthalpy turbulent boundary layer [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 528963-528963.
[13]	Jiameng SUN, Guang ZUO, Yizhe XU, Ruofan DU, Yuhong CUI. Numerical simulation of weapon delivery schemes for hypersonic vehicles in near space [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(13): 127808-127808.
[14]	Xiaodong LIU, Pengxin LIU, Chen LI, Dong SUN, Xianxu YUAN. Direct numerical simulation of high enthalpy shock wave/turbulent boundary layer interaction [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(13): 127832-127832.
[15]	XIAHOU Tangfan, CHEN Jiangtao, SHAO Zhidong, WU Xiaojun, LIU Yu. Model validation metrics for CFD numerical simulation under aleatory and epistemic uncertainty [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 25716-025716.