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International Journal of Fatigue

Volumn 23, Issue SUPPL. 1, 2001, Pages 21-30

Structural fatigue and joint degradation

(1) Terada, Hiroyuki a

a JAPAN AEROSPACE EXPLORATION AGENCY (Japan)

Author keywords

Aircraft fatigue; Corrosion; Fastener joint; Fuselage model; Service load simulation

Indexed keywords

AGING OF MATERIALS; AIRCRAFT; COMPUTER SIMULATION; CORROSION; FASTENERS; FUSELAGES; JOINTS (STRUCTURAL COMPONENTS); PNEUMATICS; STIFFNESS; STRESS ANALYSIS; SYNCHRONIZATION;

LAP JOINTS;

FATIGUE TESTING;

EID: 0035214016 PISSN: 01421123 EISSN: None Source Type: Journal
DOI: 10.1016/s0142-1123(01)00117-7 Document Type: Article

Times cited : (28)

References (12)

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2
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3
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4
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5
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- Terada, H.¹ Okada, T.²

6
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- Fatigue crack growth in riveted joints
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7
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- Fatigue of aircraft materials
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8
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- Delft University of Technology
- (1995) An experimental and analytical investigation of the fatigue behavior of fuselage riveted lap joints
- Müller, R.¹

10
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- Report No. 97-26. Sweden: Royal Institute of Technology
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- Segerfrojid, G.¹

11
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12
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- Bulging factors for predicting residual strength of fuselage panels
- (1997) Proceedings of the 19th Symposium of ICAF , vol.1 , pp. 179-196
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.