玻璃纤维增强铝合金层板高速冲击损伤容限

doi:10.7527/S1000-6893.2017.21733

Abstract

Abstract: To investigate the damage tolerance of the GLAss fiber-REinforced aluminum (GLARE) laminates subjected to high-velocity impacts, the single and multiple impact performance of the GLARE laminates was studied by tests and numerical simulation. High-velocity impact tests were conducted on GLARE panels using a one-stage gas gun at different impact locations, i.e. middle point, edge point and corner point of the plate. The ballistic limit was thus obtained as well as the failure patterns, and the dynamic response was studied based on the numerical simulation. The results show that GLARE laminates absorb the impact energy mainly in the form of plastic deformation, metal cracking, debonding, and fiber breakage. The clamp constraint exerted great influences on the damage mechanism of the GLARE laminates subjected to impacts. The failure patterns in the GLARE laminates subjected to the impact load were distinctly affected by the constraint, i.e. denting and metal cracking, plugging characteristics etc. The ballistic limit velocity of the GLARE laminates impacted at the corner point of the plate was found to be much less than that impacted at the middle location of the plate. Compared with the middle and the edge points, the corner position of the plate subjected to multiple impacts was the most vulnerable to perforation.

Key words: GLAss fiber-REinforced aluminum (GLARE) laminates, impact, constraint effect, failure pattern, ballistic limit

CLC Number:

V214.8
TP333

CHEN Yong, LIAO Gaojian, REN Lihai, LIU Xi. Damage tolerance of GLARE laminates subjected to high-velocity impact[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(7): 221733-221733.

References

[1] VOGELESANG L B, VLOT A. Development of fibre metal laminates for advanced aerospace structures[J]. Journal of Materials Processing Technology, 2000, 103(1):1-5.
[2] 孟维迎, 谢里阳, 刘建中, 等. 玻璃纤维增强铝锂合金层板单峰过载疲劳寿命性能对比研究[J]. 航空学报, 2016, 37(5):1536-1543. MENG W Y, XIE L Y, LIU J Z, et al. Contrast study on fatigue life performance of glass fiber reinforced Al-Li alloy laminates under unimodal overload[J].Acta Aeronautica et Astronautica Sinica, 2016, 37(5):1536-1543(in Chinese).
[3] 蔺晓红, 张涛, 张小波, 等. 碳纤维增强铝合金板的抗冲击性能[J]. 爆炸与冲击, 2013, 33(3):303-310. LIN X H, ZHANG T, ZHANG X B, et al. Impact resistance of carbon fiber-reinforced aluminumlaminates[J]. Explosion and Shock Waves, 2013, 33(3):303-310(in Chinese).
[4] HAMED Z, MOHADESEH F, GIANGIACOMO M, et al. Low velocity impact analysis of fiber metal laminates (FMLs) in thermal environments withvarious boundary conditions[J]. Composite Structures, 2016, 149(1):170-183.
[5] 马玉娥, 胡海威, 熊晓枫. 低速冲击下FML、铝板和复材的损伤对比研究[J]. 航空学报, 2014, 35(7):1902-1911. MA Y E, HU H W, XIONG X F. Comparison of damage in FMLs, aluminum and composite panels subjected to low-velocity impact[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(7):1902-1911(in Chinese).
[6] 万云, 章继峰, 王振清, 等. 玻纤铝合金层板受低速冲击损伤实验和仿真[J]. 哈尔滨工程大学学报, 2015, 36(6):769-773. WAN Y, ZHANG J F, WANG Z Q, et al. Low-velocity impact damage on glassfibre reinforced aluminum laminates:Experiments and finite element analysis[J]. Journal of Harbin Engineering University, 2015, 36(6):769-773(in Chinese).
[7] HEN Q, GUAN Z D, LI Z S, et al. Experimental investigation on impact performances of GLARE laminates[J]. Chinese Journal of Aeronautics, 2015, 28(6):1784-1792.
[8] YU G C, WU L Z, MA L, et al. Low velocity impact of carbon fiber aluminumlaminates[J]. Composite Structures, 2015, 119:757-766.
[9] 陶杰, 李华冠, 潘蕾, 等. 纤维金属层板的研究与发展趋势[J]. 南京航空航天大学学报, 2015, 47(5):626-636. TAO J, LI H G, PAN L, et al. Review on research and development of fiber metal laminates[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2015, 47(5):626-636(in Chinese).
[10] HU Y B, LI H G, TAO J, et al. The effects of temperature variation on mechanical behaviors ofpolyetheretherketone-based fiber metal laminates[J/OL]. Polymer Composites. (2016-05-31)[2017-11-22]. http://onlinelibrary.wiley.com/doi/10.1002/pc.24085.
[11] AHAMADI H, SABOURI H, LIAGHAT G, et al. Experimental and numerical investigation on the high velocity impact response of GLARE with different thickness ratio[J]. Procedia Engineering, 2011, 10(7):869-874.
[12] YAGHOUBI A S, LIAW B. Thickness influence on ballistic impact behaviors of GLARE 5 fiber-metal laminated beams:Experimental and numericalstudies[J]. Composite Structures, 2012, 94(8):2585-2598.
[13] ABDULLAH M R, CANTWELL W J. The impact resistance of polypropylene-basedfibre-metal laminates[J]. Composites Science and Technology, 2006, 66(11-12):1682-1693.
[14] YAGHOUBI A S, LIAW B. Effect of lay-up orientation on ballistic impact behaviors of GLARE 5 FML beams[J]. International Journal of Impact Engineering, 2013, 54(4):138-148.
[15] ZAREI H, SADIGHI M, MINAK G. Ballistic analysis of fiber metal laminates impacted by fiat and conical impactors[J]. Composite Structures, 2017, 161:65-72.
[16] RAJKUMAR G R, KRISHNA M, MURTHY H N N, et al. Experimental investigation of low velocity repeated impacts on glass fiber metal composites[J]. Journal of Materials Engineering and Performance, 2012, 21(7):1485-1490.
[17] RAJKUMAR G R, KRISHNA M, MURTHY H N N, et al. Investigation of repeated low velocity impact behavior of GFRP/aluminium and CFRP/aluminium laminates[J]. Journal of Soft Computing and Engineering, 2012, 1(6):2231-2307.
[18] MORINIÈRE F D, ALDERLIESTEN R C, TOOSKI M Y, et al. Damage evolution in GLARE fiber-metal laminate under repeated low velocity impact tests[J]. Central European Journal of Engineering, 2012, 2(4):603-611.
[19] TOOSKI M Y, ALDERLIESTEN R C, GHAJAR R, et al. Experimental investigation on distance effects in repeated low velocity impact on fiber-metal laminates[J]. Composite Structures, 2013, 99(5):31-40.
[20] BOTELHO E C, SILVA R A, PARDINI L C, et al. Review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures[J]. Materials Research, 2006, 9(3):247-256.
[21] RECHT R F, LPSON T W. Ballistic perforation dynamics[J]. International Journal of Applied Mechanics (Transactions of ASME), 1963, 30(3):384-390.
[22] JOHONSON G R, COOK W H. A constitutive model and data for metals subjected to large strains, high strain rates and high temperatures[C]//Proceedings of 7th Symposium on Ballistics. Hegue:International Ballistics Committee, 1983:541-547.
[23] HASHIN Z. Failure criteria for unidirectional fiber composites[J]. Journal of Applied Mechanics, 1980, 47(2):329-334.

Damage tolerance of GLARE laminates subjected to high-velocity impact

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