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Volumn 51, Issue , 2006, Pages

Adhesively bonded CFRP straps as fatigue crack growth retarders on AA2024-T3

Author keywords

Bonded composites; Fatigue crack retarders; Integral aircraft structure

Indexed keywords

ADHESION; AIRCRAFT; ALUMINUM; CARBON FIBERS; COMPOSITE MATERIALS; CRACK TIPS; POLYMER MATRIX; REINFORCEMENT; RESIDUAL STRESSES; STRUCTURAL PANELS;

EID: 34748899948     PISSN: 08910138     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (13)

References (18)
  • 2
    • 34748838490 scopus 로고    scopus 로고
    • National strategic technology acquisition plan for Aeronautics aviation committee; DTI report Air CB 110, 1993
    • National strategic technology acquisition plan for Aeronautics aviation committee; DTI report Air CB 110, 1993.
  • 3
    • 0038808166 scopus 로고    scopus 로고
    • Damage tolerance in Aircraft structures
    • ASTM STP 486; pp
    • C.C. Poe, Damage tolerance in Aircraft structures, ASTM STP 486; pp.79-97.
    • Poe, C.C.1
  • 4
    • 34748881906 scopus 로고    scopus 로고
    • USAF damage tolerant design handbook, AFWAL 83444, May 1984.
    • USAF damage tolerant design handbook, AFWAL 83444, May 1984.
  • 6
    • 0003536977 scopus 로고
    • A.A. Baker, R. Jones Eds, pub. Martinus Nijhoff
    • A.A. Baker, R. Jones (Eds.), Bonded Repair of Aircraft Structures, pub. Martinus Nijhoff 1988.
    • (1988) Bonded Repair of Aircraft Structures
  • 8
    • 22544435815 scopus 로고    scopus 로고
    • X. Zhang and Y. Li. AIAA Journal. 43 (7): 1613-1623, 2005.
    • (2005) AIAA Journal , vol.43 , Issue.7 , pp. 1613-1623
    • Zhang, X.1    Li, Y.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.