ARMSTRONG K B, BEVAN L G, COLE Ⅱ W F. Care and Repair of Advanced Composites[M]. 2nd ed. Warrendale:SAE international, 2005.263-265.
[2]
BELOUETTAR S, ABBADI A, AZARI Z, et al. Experimental investigation of static and fatigue behaviour of composites honeycomb materials using four point bending tests[J]. Composite Structures, 2009, 87(3):265-273.
[3]
HE Li, CHENG Yuan-sheng, LIU Jun. Precise bending stress analysis of corrugated-core, honeycomb-core and X-core sandwich panels[J]. Composite Structures, 2012, 94(5):1656-1668.
[4]
张广成, 赵景利. 蜂窝夹层结构复合材料的力学性能研究[J].机械科学与技术, 2003, 22(2):280-282.ZHANG Guang-cheng, ZHAO Jing-li. Study on mechanical properties of honeycomb sandwich structure composite[J].Mechanical Science and Technology, 2003, 22(2):280-282.
[5]
PIPES R B, ADKINS D W, DEATON J. Strength and repair of bonded scarf joints for repair of composite materials[R]. Washington:NASA, 1982.
[6]
JONES J S, GRAVES S R. Repair techniques for celion-LARC-160 graphite-polyimide composite structures[R]. Washington: NASA, 1984.
[7]
DUONG CONG N, WANG Chun-hui. Composite Repair Theory and Design[M]. Amsterdam:Elsevier, 2007.
[8]
NIU Chun-yun. Composite Airframe Structures[M]. California: AD Adaso/Adastra Engineering Center, 1992.
[9]
KUMAR S B, SRIDHAR I, SIVASHANKER S I, et al. Tensile failure of adhesively bonded CFRP composites scarf joints[J]. Materials Science and Engineering:B, 2006, 132:113-120.
[10]
KUMAR S B, SIVASHANKER S I, OSIYEMI S O, et al. Failure of aerospace composite scarf-joints subjected to uniaxial compression[J]. Materials Science and Engineering:A, 2005, 412:117-122.
[11]
TOMBLIN J S, SALAH L, WELCH J M. Bonded repair of aircraft composite sandwich structures[R]. Wichita:National Institute for Aviation Research, 2004.
[12]
TOMBLIN J S, LACY T, SMITH B, et al. Review of damage tolerance for composite sandwich airframe structures[R]. Wichita:National Institute for Aviation Research, 1999.