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Volumn 44, Issue 12, 2010, Pages 1517-1531

Permeability of various hybrid composites subjected to extreme thermal cycling and low-velocity impacts

Author keywords

Barrier layers; Fiber metal laminate; Leak

Indexed keywords

ALUMINIZED MYLAR; BARRIER LAYERS; DROP WEIGHT; EXPLORATORY STUDIES; EXTREME TEMPERATURES; FIBER METAL LAMINATES; GRAPHITE/EPOXY COMPOSITES; HYBRID COMPOSITES; IMPACT ENERGY; IMPACT LOADS; LOW VELOCITY IMPACT; PROMISING MATERIALS;

EID: 77953101470     PISSN: 00219983     EISSN: 1530793X     Source Type: Journal    
DOI: 10.1177/0021998309353957     Document Type: Article
Times cited : (8)

References (9)
  • 1
    • 0038768489 scopus 로고    scopus 로고
    • Cryocycling and mechanical testing of the cfrp for the x-33 liquid h2 fuel tank structure
    • Kessler, S., Matuxzeski, T. and McManus, H. (2001). Cryocycling and Mechanical Testing of the CFRP for the X-33 Liquid H2 Fuel Tank Structure, In: ASC 16th Technical Conference Proceedings, Blacksburg, VA, 9-12 September.
    • ASC 16th Technical Conference Proceedings
    • Kessler, S.1    Matuxzeski, T.2    McManus, H.3
  • 2
    • 70350465102 scopus 로고    scopus 로고
    • Impact damage resistance of carbon/epoxy composite tubes for the dc-xa liquid hydrogen feedline
    • Nettles, A. (1995). Impact Damage Resistance of Carbon/Epoxy Composite Tubes for the DC-XA Liquid Hydrogen Feedline, NASA Technical Paper 3583, September.
    • NASA Technical Paper 3583
    • Nettles, A.1
  • 3
    • 27644551467 scopus 로고    scopus 로고
    • Benefits of Surface Coatings for Impacted Composites to be Used for Cryogenic Tankage
    • Findley, B.C. and Johnson, W.S. (2005). Benefits of Surface Coatings for Impacted Composites to be Used for Cryogenic Tankage, AIAA Journal of Spacecrafts and Rockets, 42 (5). 804-809.
    • (2005) AIAA Journal of Spacecrafts and Rockets , vol.42 , Issue.5 , pp. 804-809
    • Findley, B.C.1    Johnson, W.S.2
  • 4
    • 0041495628 scopus 로고    scopus 로고
    • Gas permeation of fiber reinforced plastics
    • Humpenoder, J. (1998). Gas Permeation of Fiber Reinforced Plastics, Cryogenics, 38 (1). 143-147.
    • (1998) Cryogenics , vol.38 , Issue.1 , pp. 143-147
    • Humpenoder, J.1
  • 6
    • 0036497729 scopus 로고    scopus 로고
    • Prediction of low velocity impact damage in carbon-epoxy laminates
    • de Moura, M. and Marques, A. (2000). Prediction of Low Velocity Impact Damage in Carbon-Epoxy Laminates, Composites: Part A, 33: 361-368.
    • (2000) Composites: Part A , vol.33 , pp. 361-368
    • De Moura, M.1    Marques, A.2
  • 8
    • 0031696798 scopus 로고    scopus 로고
    • Low-velocity impact damage in laminated composite materials, impact response and dynamic failure of composites and laminate materials
    • Wang, H. and Vu-Kanh, T. (1998). Low-velocity Impact Damage in Laminated Composite Materials, Impact Response and Dynamic Failure of Composites and Laminate Materials, Key Engineering Materials, 141-143: 277-304.
    • (1998) Key Engineering Materials , vol.141-143 , pp. 277-304
    • Wang, H.1    Vu-Kanh, T.2
  • 9
    • 0033685166 scopus 로고    scopus 로고
    • Delamination threshold loads for low velocity impact on composite laminates
    • Schoeppner, G. and Abrate, S. (2000). Delamination Threshold Loads for Low Velocity Impact on Composite Laminates, Composites: Part A, 31: 903-915.
    • (2000) Composites: Part A , vol.31 , pp. 903-915
    • Schoeppner, G.1    Abrate, S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.