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Composite Structures

Volumn 57, Issue 1-4, 2002, Pages 453-458

Bonded repairs to rib stiffened wing skins

(3) Jones, R a Whittingham, B a Marshall, I H a

a MONASH UNIVERSITY (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

FINITE ELEMENT METHOD; REPAIR; STRUCTURAL DESIGN;

METALLIC SKINS;

COMPOSITE STRUCTURES;

DESIGN;

EID: 0036659013 PISSN: 02638223 EISSN: None Source Type: Journal
DOI: 10.1016/S0263-8223(02)00113-7 Document Type: Article

Times cited : (8)

References (13)

1
- 0019392130
- An application of the inclusion analogy for bonded reinforcements
- (1981) Int J Solid Struct , vol.17 , pp. 827-838
- Rose, L.R.F.¹

2
- 0033303914
- Composite repairs to rib stiffened panels
- (1999) J Compos Struct , vol.47 , pp. 737-744
- Ting, T.¹ Jones, R.² Chiu, W.K.³ Marshall, I.H.⁴ Greer, J.⁵

3
- 0003689589
- Dr. thesis. Delft University of Technology. June
- (1994) Damage Tolerant Repair Techniques for Pressurized Aircraft Fuselages
- Fredell, R.S.¹

4
- 0003536977
- Dordrecht: Martinus Nijhoff
- (1988) Bonded Repair of Aircraft Structures
- Baker, A.A.¹ Jones, R.²

5
- 0003768837
- DSTO, Melbourne. DSTO-TN-0067
- (1997) Finite Element Analysis of an F-111 Lower Wing Skin Fatigue Crack Repair
- Callinan, R.J.¹ Sanderson, S.² Keeley, D.³

6
- 0004023422
- Sandia Report, SAND98-1015, February
- (1999) Full Scale Structural and NDI Validation Tests of Bonded Composite Doublers for Aircraft Applications
- Roach, D.¹ Walkington, P.²

7
- 0004023422
- Sandia National Laboratories/Department of Energy. Sandia Report, SAND98-1016, August
- (1998) Damage Tolerance Assessment of Bonded Composite Doublers for Commercial Aircraft Applications
- Roach, D.¹

8
- 0024776670
- Structural aspects of the design of an all boron/epoxy reinforcement for the F-111C wing pivot fitting
- (1989) J Compos Struct , vol.11 , Issue.1 , pp. 57-83
- Molent, L.¹ Callinan, R.J.² Jones, R.³

9
- 0032686270
- Composite repairs to cracks in thick metallic components
- in press
- J. Compos. Struct
- Jones, R.¹ Chiu, W.K.² Sawyer, J.P.G.³

10
- 0004061968
- Internal Report, HQ USAF Academy/ADFEM, February
- (1999) The Fatigue Characteristics of Repaired and Unrepaired C141 Panels
- Massar, J.J.A.¹

11
- 0003318627
- Composite repairs to cracked holes under biaxial loading
- Melbourne, Australia, November J. Compos. Struct., in press
- (2001) Proceedings ICCS11
- Jones, R.¹ Peng, D.²

12
- 84940853549
- Numerical analysis and design
- Baker AA. Rose LRF, Jones R, editors. Oxford: Elsevier Applied Science Publishers; [Chapter 9]
- (2002) Advances in the Bonded Composite Repair of Metallic Airframe Structures
- Jones, R.¹

13
- 2142782514
- December
- (1983) Damage Tolerance Design Handbook , vol.4

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.