SCOPUS 정보 검색 플랫폼

Fatigue and Fracture of Engineering Materials and Structures

Volumn 24, Issue 10, 2001, Pages 677-686

A model to assess the fatigue behaviour of ageing aircraft fuselage

(4) Diamantakos, I D a Labeas, G N b Pantelakis, Sp G a Kermanidis, Th B a

a UNIVERSITY OF PATRAS (Greece)

b ISTRAM (Greece)

Author keywords

Butt joint; Crack initiation; Fatigue crack growth; Lap joint; Multiple site damage

Indexed keywords

AGING OF MATERIALS; COMPUTER SIMULATION; CRACK INITIATION; CRACK PROPAGATION; FINITE ELEMENT METHOD; FUSELAGES; JOINTS (STRUCTURAL COMPONENTS); MATHEMATICAL MODELS; STRUCTURAL LOADS;

BUTT JOINTS;

FATIGUE TESTING;

EID: 0035471190 PISSN: 8756758X EISSN: None Source Type: Journal
DOI: 10.1046/j.1460-2695.2001.00423.x Document Type: Article

Times cited : (11)

References (23)

1
- 0000079948
- Investigation of fuselage structure subjected to widespread fatigue damage
- DOT/FAA/AR-97-2, (Edited by C. Bigelow). National Technical Information Service, Springfield, VA, USA
- (1996) Proceedings of FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures , pp. 439-460
- Gruber, M.L.¹ Wilkins, K.E.² Worden, R.E.³

2
- 0346335856
- Tailoring the structural integrity process to meet the challenges of aging aircraft
- (1999) Int. J. Fatigue , vol.21 , pp. 1-14
- Simpson, D.L.¹ Brooks, C.L.²

3
- 0033894246
- Strength of 2024-T3 aluminium panels with multiple site damage
- (2000) J. Aircraft , vol.37 , pp. 325-331
- Smith, B.L.¹ Saville, P.A.² Mouak, A.³ Myose, R.Y.⁴

4
- 1842508896
- Atlanta, Georgia, August 28-30, (Edited by C. Bigelow). National Technical Information Service, Springfield, VA, USA
- (1996) Proceedings of FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures , pp. 129
- Inman, M.E.¹ Kelly, R.G.² Willard, S.A.³ Piascik, R.S.⁴

5
- 0031335576
- Fatigue damage in aging aircraft
- (1997) Engng Failure Anal. , vol.4 , pp. 237-257
- Pitt, S.¹ Jones, R.²

6
- 0002682481
- The characterization of widespread fatigue damage in fuselage
- FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, (Edited by C. E. Harris). Neuilly-Sur-Seine, France
- (1994) NASA CP , vol.3272 , pp. 563-580
- Piascik, R.S.¹ Willard, S.A.² Miller, M.³

7
- 0003420977
- Prentice Hall, Englewood Cliffs, NJ, USA
- (1990) Fundamentals of Metal Fatigue Analysis
- Bannantine, J.A.¹ Corner, J.J.² Handrock, J.L.³

8
- 0002582006
- Doc. no. TR-2.1-04-1.3/AS. Aerospatiale Toulouse, France
- (1997) Structural Maintenance of Ageing Aircraft: Theoretical Models-Initiation Problem
- Santgerma, A.¹ Balzano, M.²

9
- 0029212934
- Fatigue crack growth of retardation assessment of T2024-T3 and 6061-T6 aluminum specimens
- (1995) Theoret. Appl. Fract. Mech. , vol.22 , pp. 35-42
- Pantelakis, Sp.G.¹ Kermanidis, Th.B.² Pavlou, P.G.³

10
- 0004019913
- Paris Production, St. Louis, MO, USA
- (1985) The Stress Analysis of Cracks Handbook, 2nd edn.
- Tada, H.¹ Paris, P.² Irwin, G.³

11
- 0003878724
- Pergamon Press, Oxford, UK
- (1991) Weight Functions and Stress Intensity Factors Solutions
- Wu, X.R.¹ Carlsson, A.J.²

12
- 0642353471
- Computational Mechanics Publications, Southampton, UK
- (1996) Database of Stress Intensity Factors, Software by G.F.L. Lopez
- Aliabadi, M.H.¹

13
- 0001035714
- Multiple-site-damage in 2024-T3 alloy sheet
- (1992) Int. J. Fatigue , vol.15 , pp. 293-299
- Pártl, O.¹ Schijve, L.²

14
- 0002475030
- Royal Aircraft Establishment, Technical Report 81144. Defence Research Agency, Farnborough, UK
- (1981) Stress Intensity Factors for Cracks at Fastener Holes in a Row of Fastener Holes
- Rooke, D.P.¹

15
- 0002656934
- A concept for the evaluation of MSD based on probabilistic assumptions
- AGARD-CP-568. RTO/NATO, Neuilly-Sur-Seine, France
- (1995) Widespread Fatigue Damage in Military Aircraft , pp. 61-612
- Horst, P.¹ Schmidt, H.J.²

16
- 0015110427
- On the finite element method for calculating stress intensity factors for cracked plates in bending
- (1971) Engng Fract. Mech. , vol.3 , pp. 161-177
- Wilson, W.K.¹ Tomson, D.G.²

17
- 0002568710
- Widespread fatigue damage and single member failure prediction of military jet trainers of Czech design and production
- AGARD-CP-568. RTO/NATO, Neuilly-Sur-Seine, France
- (1995) Widespread Fatigue Damage in Military Aircraft , pp. 41-411
- Fidransky, J.¹ Fiala, J.²

18
- 0342626770
- Multiple site damage in riveted lap-joints: Experimental simulation and finite elements prediction
- (2000) Int. J. Fatigue , vol.22 , pp. 319-338
- Silva, L.F.M.¹ Goncalves, J.P.M.² Oliveira, F.M.F.³ De Castro, P.M.S.T.⁴

19
- 0003613155
- Prentice Hall Int., London
- (1993) Mechanical Behaviour of Materials , pp. 369
- Dowling, N.¹

20
- 0002649902
- SMAAC-WP-5.2-06-1.3/AEM. Aermacchi, Varese, Italy
- (1998) Round Robin Programme, Sub-task 5.2, Numerical Round Robin Test Type III, Crack Growth Test Results
- Cattaneo, G.¹

21
- 0002724476
- Fatigue initiation in unnotched specimens subjected to monotonic and cyclic loading
- (1984) Theoret Appl. Fract. Mech. , vol.2 , pp. 67-73
- Sih, G.C.¹ Chao, C.K.²

22
- 0002562864
- SMAAC-WP-5-ZZ-1.3. IDMEC. IDMEC, Porto, Portugal
- (1998) Results of Task 5 Problems 'type II' (lap-joint msd growth) and 'type V' (lap-joint residual strength) of Round Robin Programme - A Comparison
- Domingues, J.S.¹ Silva, L.M.² De Castro, P.T.³

23
- 0002568249
- BRITE-EURAM, No. BE 95-1053, Final Report. CEC, Brussels, Belgium
- (1996) Structural Maintenance of Ageing Aircraft

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.