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Volumn 23, Issue SUPPL. 1, 2001, Pages 337-347

Fatigue and corrosion in aircraft pressure cabin lap splices

Author keywords

Aircraft pressure cabins; Corrosion; Fatigue

Indexed keywords

CORROSION; CRACK PROPAGATION; FATIGUE OF MATERIALS; FATIGUE TESTING;

EID: 0035207018     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0142-1123(01)00147-5     Document Type: Article
Times cited : (22)

References (24)
  • 2
    • 21844465827 scopus 로고
    • Fractographic analysis of longitudinal fuselage lapjoint at stringer 42 of Fokker 100 full scale test article TA15 after 126250 simulated flights
    • Amsterdam: Fokker Aircraft Ltd, November
    • (1994) Fokker Report , vol.RT2160
    • Eijkhout, M.T.1
  • 4
    • 85002050056 scopus 로고
    • Structural airworthiness of aging Boeing jet transport - 747 fuselage fatigue test program
    • AIAA 92-1128. Washington, DC: American Institute of Aeronautics and Astronautics, February
    • (1992) 1992 Aerospace Design Conference
    • Gopinath, K.V.1
  • 6
    • 85031600315 scopus 로고
    • Fracture mechanics analysis of short cracks at loaded holes
    • Behaviour of Short Cracks in Airframe Components, Neuilly-sur-Seine: Advisory Group for Aerospace Research and Development
    • (1983) AGARD Conference Proceedings , vol.328 , pp. 81-86
    • Rooke, D.P.1
  • 7
    • 0025436108 scopus 로고
    • Corrosion fatigue crack arrest in aluminium alloys
    • Quantitative methods in fractography, editors B.M. Strauss and S.K. Putatunda, American Society for Testing and Materials, Philadelphia, Pensylvania
    • (1990) ASTM STP , vol.1085 , pp. 144-165
    • Wanhill, R.J.H.1    Schra, L.2
  • 10
    • 0006938717 scopus 로고    scopus 로고
    • Fractography of MSD in fuselage lap splices
    • Brite Euram Project No. BE95-1053, SMAAC: Structural Maintenance of Ageing Aircraft, Document No. SMAAC-TR-1.3-02-1.3/NLR, National Aerospace Laboratory, Amsterdam, July
    • (1998) NLR Technical Report TR 98310
    • Wanhill, R.J.H.1
  • 16
    • 85031607967 scopus 로고
    • The effect of cladding condition on the stages of fatigue crack formation and growth
    • Branger J., Berger F., editors, Problems with Fatigue in Aircraft, Emmen: Swiss Federal Aircraft Establishment (F+W)
    • (1975) Proceedings of the Eighth ICAF Symposium , pp. 251-2523
    • Forsyth, P.J.E.1
  • 19
    • 0004022391 scopus 로고
    • Short-crack growth behaviour in an aluminium alloy - An AGARD cooperative test programme
    • Neuilly-sur-Seine: Advisory Group for Aerospace Research and Development
    • (1988) AGARD Report , vol.732
    • Newman J.C., Jr.1    Edwards, P.R.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.