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Radial braiding과 RTM공법을 적용한 항공기용 CFRP hat stringer 설계 및 이의 물성 = Design and properties of CFRP hat stringer for aircraft applications by radial braiding and RTM method

천진성 2020년

논문상세정보
인용/피인용
' Radial braiding과 RTM공법을 적용한 항공기용 CFRP hat stringer 설계 및 이의 물성 = Design and properties of CFRP hat stringer for aircraft applications by radial braiding and RTM method' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • 일반 연속간행물
  • Aircraft
  • Hat stringer
  • Radial braiding
  • cfrp
  • rtm
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
1,371 0

0.0%

' Radial braiding과 RTM공법을 적용한 항공기용 CFRP hat stringer 설계 및 이의 물성 = Design and properties of CFRP hat stringer for aircraft applications by radial braiding and RTM method' 의 참고문헌

  • 항공우주용 복합재료 기술
    정의경 섬유소재솔류션센터 심층보고 서 [2015]
  • 탄소섬유를 다양한 복합재료에 응용하기 위한 연구개발 동향
    양갑승 섬유기술과산업, 16(3) [2012]
  • 복합재료 항공기의 등장과 기술적 당면과 제의 검토
    최원종 최흥섭 황명래 한국방위산업학회 제16권 제2호 [2009]
  • “Electrical and the Mechanical Properties of Graphite particle/Carbon fiber hybrid Conductive Polymer Composites”
    Han, K.S. Heo, S.I. Oh, K.S. Yun, J.C. 『한국복합재료학회지』, 제19권, 제2호 [2006]
  • Visualization of Guided Wave Propagation by Ultrasonic Imaging Methods
    [2007]
  • Twoand Three-dimensional Isogeometric Cohesive Elements for Composite Delamination Analysis
    Vol . 60 , 193-212 [2014]
  • Triaxially braided materials for composites , in : Composite Materials Series 3—Textile Structural Composites
    pp . 117–28 [1989]
  • The effect of adding carbon nanotubes to glass/epoxy composites in the fibre sizing and/or the matrix ,
    41 , 532-538 , [2010]
  • The Effects of Stitch Orientation on the Tensile and Open Hole Tension Properties of Carbon/epoxy Plain Weave Laminates
    Vol . 35 , 563-571 [2012]
  • Study on the mechanical properties of jute/glass fiber -reinforced unsaturated polyester hybrid composites : Effect of surface modification by ultraviolet radiation , J. Reinf
    25 , 575-588 [2006]
  • Study on Through the Thickness Stresses in the Corner Radius of a Laminated Composite Structure
    Vol . 41 , No . 8 , 665-672 [2013]
  • Structural health monitoring techniques for aircraft composite structures
    46 , 342-352 [2010]
  • Structural Health Monitoring ( SHM ) , A Future Alternative toConventional NDT ''
    [2006]
  • Strength prediction of a triaxially braided composite.
    Vol . 42 , Issue 8 , 1000-1006 [2011]
  • Strength analysis of three dimensional braided T-shaped composite structures.
    pp . 162-168 [2009]
  • Stiffness degradation model for biaxial braided composites under fatigue loading.
    Vol 39 , Issue 3 , 548-555 [2008]
  • Rate dependentCompressive response of 2D tri-axially braidedCarbon fiberComposites and the effects of resin on the interfacial shear strength.
    Vol . 40 , 19-27 [2009]
  • Open Hole Quasi-static and Fatigue Characterization of 3D Woven Composites
    Vol . 131 , 2015 , pp . 765-774 [2011]
  • Multiscale Damage Modelling of 3D Weave Compsite by Asymptotic Homogenization ,
    Vol . 95 , 105-113 [2013]
  • Monitoring of fibre reinforced composites with embedded optical fibre Bragg sensors , with application to filament wound pressure vessels
    34 , 289-296 [2001]
  • Mode I interlaminar fracture behavior and mechanical properties of CFRPs with nanoclay-filled epoxy matrix
    38 , 449-460 [2007]
  • Mechanical properties of carbon fiber reinforced epoxy/clay nanocomposites
    68 , 854-861 [2008]
  • Mechanical performance of 2-D braided carbon epoxy composites
    Vol . 3538 , 253-265 [1998]
  • Low velocity impact of combination Kevlar/carbon fiber sandwich composites
    69 , 396-406 [2005]
  • Lightning Direct Effects Handbook , AGATE-WP3.1 -031027
    [2002]
  • L. C. Pardini , and M. C. Rezende , A review on the development and properties of continuous fiber/ epoxy/aluminum hybrid composites for aircraft structures
    9 , 247-256 [2006]
  • Jr.1,3,4 Design and Fabrication of VARTM Fabricated Skin Panels with Integrated Hollow Hat Stiffeners
    [2014]
  • Influence of carbon nanotube reinforcement on the processing and the mechanical behaviour of carbon fiber/epoxy composites
    47 , 2914-2923 [2009]
  • Influence of 3D braiding technology parameters on tensile properties of composites
    30 ( 1 ) , 55-58
  • Improvements in mechanical properties of a carbon fiber epoxy composite using nanotube science and technology
    92 , 2653-2662 [2010]
  • Impact Properties of Laminated Composites with Stitching with Stitching Fibers
    Vol . 76 , 21-27 [2006]
  • Health Monitoring of Aerospace Structures Smart Sensor Technologies and Signal Processing
    [2004]
  • Handbook of Technical Textiles , ” by A. R. Horrocks
    [2000]
  • H. Hamada and Z. Makawa , Integrated braided composite technology : simulation– abrication–strength
    [1994]
  • Fabrication of 3D Textile Preforms by Multi-layer Weaving
    [1997]
  • Enhancing thermal conductivity of glass fiber/polymer composites through carbon nanotubes incorporation ,
    41 , 533-536 [2010]
  • Encyclopedia of Structural Health Monitoring , 1st ed.
    [2009]
  • Eddy current holography evaluation of delamination in carbonepoxy composites
    43 , 260-264 [2001]
  • Development of Stitched , Braided and Woven Composite Structures in the ACT Program and at Langley Research Center
    [1997]
  • Damage Behavior of fiber reinforced composite plates subjected to drop weight impacts
    66 , 61-68 [2006]
  • Composite Structures , Design , Safety and Innovation
    [2005]
  • Characterization and manufacture of braided composites for large commercial aircraft structure.
    [1991]
  • CFRP using braided preforms/RTM process for aircraft applications
    Vol . 14 , Issue 4 , 365-383 [2005]
  • CFRP using braided preform/RTM process for aircarft applications
    Vol . 14 , No . 4 , 365-83 [2005]
  • Braiding : from cordage to composites.
    [2016]
  • Biofibres and biocomposites
    71 , 343-364 [2008]
  • Analysis of Regulatory Guidance for Health Monitoring
    [2000]
  • An Assessment of the State-of- the-Art in the Design and Manufacturing of Large Composite Structures for Aerospace Vehicles
    [2001]
  • Aircraft Lightning Protection Handbook
    [1989]
  • Advanced braiding technology and Muratec braider
    [1994]
  • Accelerated thermal ageing of epoxy resin and 3D carbon fiber/epoxy braided composites.
    Vol . 85 , 13-171 [2016]
  • A study of quadriaxial and triaxial composites tubes developed by braid winding.
    [2013]
  • A Mechanistic Interpretation of the Comparative in-plane Mechanical Properties of 3D Woven , Stitched and Pinned Composites
    Vol . 41 , 709-728 [2010]
  • 9. P. D. Mangalgiri, Composite materials for aerospace applications, Bull. Mater. Sci., 22, 657-664, 1999.
  • 79. A. Mungalov and A. Bogdanovich, Complex shape 3-D braided composite Preforms:structural shapes for marine and aerospace, SAMPE Journal 40, 7–1, 2004.
  • 74. H. Pıhtılı and N. Tosun, Effect of load and speed on the wear behaviour of woven glass fabrics and aramid fibre -reinforced composites, Wear, 252, 979-984, 2002.
  • 72. P. Cawley and R. D. Adams, Sensitivity of the coin-tap method of nondestructive testing, Mater. Eval., 47, 558-563, 1989.
  • 57. C. Soutis, Fibre reinforced composites in aircraft construction, Prog. Aerosp. Sci., 41, 143-151, 2005.
    41 , 143-151 [2005]
  • 54. M. H. G. Wichmann, J. Sumfleth, F. H. Gojny, M. Quaresimin, B. Fiedler, and K. Schulte, Glass-fibre-reinforced composites with enhanced mechanical and electrical properties benefits and limitations of a nanoparticle modified matrix, Eng. Fract. Mech., 73, 2346-2359, 2006.
    73 , 2346-2359 [2006]
  • 51. C. Soutis, Carbon fiber reinforced plastics in aircraft construction, Mater. Sci. Eng. A-Struct. Mater. Prop. Microstruct., 412, 171-176, 2005.
    412 , 171-176 [2005]
  • 50. K. Imielinska and L. Guillaumat, The effect of water immersion ageing on low-velocity impact behaviour of woven aramid-glass fibre/epoxy composites, Compos. Sci. Technol., 64, 2271-2278, 2004.
  • 48. C. Soutis, Fibre reinforced composites in aircraft construction, Prog. Aerosp. Sci., 41, 143-151, 2005.
    41 , 143-151 [2005]
  • 38. S. W. Beckwith and C. R. Hyland, Resin transfer molding: a decade of technology advances, SAMPE Journal 34, 7–9, 1998.
  • 34. C. M. Pastore and F. K. Ko,Modelling of textile structural composites, Part I: Processing-science model for three -dimensional braiding, J. Textile Inst. 81, 480–90, 1990.
  • 33. N. Khokar, 3-D weaving: theory and practice, J. Textile Inst. 92, 193–07, 2001.
  • 32. T. Uozumi and M. Hirukawa, Braiding technologies for commercial applications, in: 6th Jap. Int’ SAMPE Symposium, 497–500, 1999.
  • 30. H. B. Dexter, Innovative textile reinforced composite materials for aircraft structures, in: 28th Int’ SAMPE Tech. Conf., 404–16, 1996.
    [1996]
  • 29. A. Mungalov and A. Bogdanovich, Complex shape 3-D braided composite Preforms:structural shapes for marine and aerospace, SAMPE Journal 40, 7–1, 2004.
  • 28. K.S. Willden, C. G. Harris, B. W. Flynn, M. G. B. Scholz, S. Stawski, and V. Wiriston The boeing Company Seattle, Washington, Advance Technology Composite Fuselage- Manufacturing NASA Contractor Report 4735, 2015.
    [2015]
  • 26. Aircraft Lightning Zoning, SAE ARP (Aerospace Recommended Practice) 5414, SAE Publications, USA, 2000.
  • 25. Branscomb, D., Beale, D., Broughton, R., “New directions in braiding,” Journal of Engineered Fibers and Fabrics, Vol. 8, Issue 2, 11-24. 2013.
  • 22. Zhang MZ, Li HJ, Li KZ (2004) Progressing in the study on mechanical properties of the 3D braided composites. J Materials Eng, [2], 44-48, 2014.
  • 18. Achenbach, J.D., "QNDE and SHM for Commercial Aircraft", Seminar at KoreanAir R&D Center, 19 May 2009.
  • 11. P. D. Mangalgiri, Composite materials for aerospace applications, Bull. Mater. Sci., 22, 657-664, 1999.