Jones J S,Graves S R.Repair techniques for Celion/LARC2160 graphite/ polyimide composite structures [R].NASA-CR-3794,1984
[5]
Dean G,Crocker L.The use of finite element methods for design with adhesives [M].London:National Physical Laboratory,2001
[6]
Charalambides M N,Kinloch A J,Natthews F L.Adhesively-bonded repairs to fiber-composite materials Ⅱ:finite element modelling [J].Composite Part A:Applied Science and Manufacturing,1998,29(11):1383-1396
[7]
Jones J S,Graves S R.Repair techniques for Celion/LARC2160 graphite/ polyimide composite structures [R].NASA-CR-3794,1984
[8]
Kumar S B,Sivashanker S.Failure of aerospace composite scarf-joints subjected to uniaxial compression [J].Materials Science and Engineering A,2005,412(1):117-122
[9]
Wang C H,Gunnion A J.On the design methodology of scarf repairs to composite laminates [J].Composite Science and Technology,2008,68(1):35-46
[10]
Charalambides M N,Kinloch A J,Natthews F L.Adhesively-bonded repairs to fiber-composite materials Ⅱ:finite element modelling [J].Composite Part A:Applied Science and Manufacturing,1998,29(11):1383-1396
[11]
Zgoul M,Crocombe A D.Numerical modeling of lap joints bonded with a rate-dependent adhesive [J].International Journal of Adhesion & Adhesives,2004,24:355-366
[12]
Kumar S B,Sivashanker S.Failure of aerospace composite scarf-joints subjected to uniaxial compression [J].Materials Science and Engineering A,2005,412(1):117-122
[13]
Dean G.Modeling non-linear creep behavior of an epoxy adhesive [J].International Journal of Adhesion & Adhesives,2007,27:636-646
[14]
Wang C H,Gunnion A J.On the design methodology of scarf repairs to composite laminates [J].Composite Science and Technology,2008,68(1):35-46
[15]
Zgoul M,Crocombe A D.Numerical modeling of lap joints bonded with a rate-dependent adhesive [J].International Journal of Adhesion & Adhesives,2004,24:355-366
[16]
Yu X X,Crocombe A D.Material modeling for rate-dependent adhesives [J].International Journal of Adhesion & Adhesives,2001,21:197-210
[17]
Dean G.Modeling non-linear creep behavior of an epoxy adhesive [J].International Journal of Adhesion & Adhesives,2007,27:636-646
[18]
Tserpes K I,Labeas G.Strength prediction of bolted joints in graphite/epoxy composite laminates [J].Composite Part B:Engineering,2002,33(7):521-529
[19]
Yu X X,Crocombe A D.Material modeling for rate-dependent adhesives [J].International Journal of Adhesion & Adhesives,2001,21:197-210
[20]
Change F K,Springer G S.The strengths of fiber reinforced composite bends [J].Composite Material,1986,20(1):30-45
[21]
Tserpes K I,Labeas G.Strength prediction of bolted joints in graphite/epoxy composite laminates [J].Composite Part B:Engineering,2002,33(7):521-529
[22]
Change F K,Springer G S.The strengths of fiber reinforced composite bends [J].Composite Material,1986,20(1):30-45
[23]
Tserpes K I,Papanikos P,Kermanidis Th.A three-dimensional progressive damage model for bolted joints in composite laminates subjected to tensile loading [J].Fatigue & Fracture of Engineering Materials & Structures,2002,24(10):663-675
[24]
Tserpes K I,Papanikos P,Kermanidis Th.A three-dimensional progressive damage model for bolted joints in composite laminates subjected to tensile loading [J].Fatigue & Fracture of Engineering Materials & Structures,2002,24(10):663-675
[25]
Hashin Z.Failure criteria for unidirectional fibre composites[J].Journal of Applied Mechanics,1980,47:329-334
[26]
Tan S C,Perez J.Progressive failure of laminated composites with a hole under compressive loading [J].Journal of Reinforced Plastics and Composites,1993,12(10):1043-1057
[27]
Hashin Z.Failure criteria for unidirectional fibre composites[J].Journal of Applied Mechanics,1980,47:329-334
[28]
Riccio A,Scaramuzzino F.Embedded delamination growth in composite panels under compressive load [J].Composites Part B:Engineering,2001,32(3):209-218
[29]
中国航空研究院.中国航空材料手册[M].2版.北京:航空工业出版社,2006 Chinese Aviation Research Institute.China aeronautical materials handbook[M]. 2nd ed.Beijing:Aviation Industry Press,2006
[30]
Tan S C,Perez J.Progressive failure of laminated composites with a hole under compressive loading [J].Journal of Reinforced Plastics and Composites,1993,12(10):1043-1057
[31]
Riccio A,Scaramuzzino F.Embedded delamination growth in composite panels under compressive load [J].Composites Part B:Engineering,2001,32(3):209-218
[32]
中国航空研究院.中国航空材料手册[M].2版.北京:航空工业出版社,2006 Chinese Aviation Research Institute.China aeronautical materials handbook[M]. 2nd ed.Beijing:Aviation Industry Press,2006
[33]
喻梅,许希武.复合材料挖补修理结构的压缩强度分析[J].中国矿业大学学报,2008,37(5):711-714 Yu Mei,Xu Xiwu.Study of the compression strength of scarf patch repaired composite structures [J].Journal of China University of Mining & Technology,2008,37(5):711-714(in Chinese)
[34]
喻梅,许希武.复合材料挖补修理结构的压缩强度分析[J].中国矿业大学学报,2008,37(5):711-714 Yu Mei,Xu Xiwu.Study of the compression strength of scarf patch repaired composite structures [J].Journal of China University of Mining & Technology,2008,37(5):711-714(in Chinese)
[35]
Mortensen F,Thomsen O T.Analysis of adhesive bonded joints:a unified approach [J].Composites Science and Technology,2002,62(7):1011-1031
[36]
Mortensen F,Thomsen O T.Analysis of adhesive bonded joints:a unified approach [J].Composites Science and Technology,2002,62(7):1011-1031
[37]
Kafkalidis M S,Thouless M D.Deformation and fracture of adhesive layers constrained by plastically-deforming adherents [J].Adhesion Science and Technology,2000,14(13):1593-1607
[38]
Kafkalidis M S,Thouless M D.Deformation and fracture of adhesive layers constrained by plastically-deforming adherents [J].Adhesion Science and Technology,2000,14(13):1593-1607