SCOPUS 정보 검색 플랫폼

Composites - Part A: Applied Science and Manufacturing

Volumn 32, Issue 9, 2001, Pages 1255-1262

The behaviour of damage tolerant hat-stiffened composite panels loaded in uniaxial compression

(1) Falzon, Brian G a

a IMPERIAL COLLEGE LONDON (United Kingdom)

Author keywords

C. finite element analysis (FEA); Postbuckling

Indexed keywords

BOUNDARY CONDITIONS; BUCKLING; COMPRESSION TESTING; FINITE ELEMENT METHOD; SHEAR DEFORMATION; STIFFNESS; STRAIN MEASUREMENT; STRUCTURAL LOADS; STRUCTURAL PANELS;

HAT-STIFFENED COMPOSITE PANELS; POSTBUCKLING DESIGNS;

COMPOSITE STRUCTURES;

EID: 0035447679 PISSN: 1359835X EISSN: None Source Type: Journal
DOI: 10.1016/S1359-835X(01)00074-4 Document Type: Article

Times cited : (42)

References (22)

1
- 0003554383
- Postbuckling behavior of selected flat stiffened graphite-epoxy panels loaded in compression
- (1982) AIAA J Paper , vol.82 , Issue.777 , pp. 464-478
- Starnes J.H., Jr.¹ Knight, N.F.² Rouse, M.³

2
- 0029277510
- Buckling and postbuckling of composite structures
- (1995) Composites , vol.26 , Issue.3 , pp. 189-199
- Stevens, K.A.¹ Ricci, R.² Davies, G.A.O.³

3
- 0003201649
- Postbuckling failure of a blade-stiffened carbon-epoxy compression panel
- 5-9 July, Paris, France
- (1999) 12th International Conference on Composite Materials (ICCM-12)
- Falzon, B.G.¹ Stevens, K.A.² Goia, M.³ Davies, G.A.O.⁴

4
- 0022808555
- Experimental investigation on advanced composite-stiffened structures under uniaxial compression and bending
- (1986) AIAA J , vol.24 , Issue.11 , pp. 1823-1830
- Romeo, G.¹

5
- 0022940932
- ICAS-86-4.2.1
- (1986) The design and construction of a post buckled carbon fibre wing box structure , pp. 238-243
- Brooks, W.G.¹

6
- 0027879679
- The effects of manufacturing methods on the buckling and postbuckling strength of thin-skinned carbon-fibre composite panels, advanced composites '93
- Wollongong, Australia, January
- (1993) International Conference on Advanced Composite Materials
- Falzon, B.G.¹ Steven, G.P.²

7
- 0031079137
- Buckling mode transition in hat-stiffened composite panels loaded in uniaxial compression
- (1997) Compos Struct , vol.37 , Issue.2 , pp. 253-267
- Falzon, B.G.¹ Steven, G.P.²

8
- 0028336467
- Buckling and failure characteristics of compression-loaded stiffened composite panels with a hole
- (1994) Compos Struct , vol.28 , Issue.1 , pp. 1-17
- Nagendra, S.¹ Gürdal, Z.² Haftka, R.T.³

9
- 0023983992
- Buckling behavior of compression-loaded symmetrically laminated angle-ply plates with holes
- (1988) AIAA J , vol.26 , Issue.3 , pp. 330-336
- Nemeth, M.P.¹

10
- 85002811160
- Buckling and postbuckling behavior of square compression loaded graphite-epoxy plates with circular cutouts
- (1990) NASA Technical Paper , vol.3007
- Nemeth, M.P.¹

11
- 0003725211
- PhD thesis, Department of Aeronautical Engineering, University of Sydney, Australia
- (1995) An investigation into the buckling and postbuckling behaviour of hat-stiffened composite panels
- Falzon, B.G.¹

12
- 0028391921
- Analysis of the snap phenomenon in buckled plates
- (1994) Int J Non-Linear Mech , vol.29 , Issue.2 , pp. 123-138
- Stoll, F.¹

13
- 0003836452
- Loads and deformations of buckled rectangular plates
- (1959) NASA Technical Report , vol.R-40
- Stein, M.¹

14
- 0016569518
- Buckling and post-buckling behaviour of plates with holes
- (1975) Aeronautical Quarterly , vol.26 , pp. 281-296
- Ritchie, D.¹ Rhodes, J.²

15
- 0022925004
- A four node Marguerre element for non-linear shell analysis
- (1986) Engng Comput , vol.3 , Issue.4 , pp. 276-282
- Jettour, P.¹ Frey, F.²

16
- 0003554385
- Finite element analysis of geometrically non-linear problems using a corotational large rotation formulation
- (1990) University of Sydney Aeronautical Technical Note , vol.9001
- McIvor, J.D.C.¹ Steven, G.P.²

17
- 0028595202
- Factors influencing nonlinear static response prediction and test-analysis correlation for composite panels
- (1994) Compos Struct , vol.29 , Issue.1 , pp. 13-25
- Knight N.F., Jr.¹

18
- 0003609373
- England: Wiley
- (1997) Non-linear finite element analysis of solids and structures , vol.1
- Crisfield, M.A.¹

19
- 4244013333
- Department of Aeronautics, Imperial College of Science, Technology and Medicine, London
- (1988) Failure prediction of thick structural composites, progress report 3
- Falzon, B.G.¹ Hitchings, D.² Stevens, K.A.³ Davies, G.A.O.⁴

20
- 15944377201
- (1997) Optimization of stiffened panels in which mode jumping is accounted for. AIAA Paper , vol.97 , Issue.1141 , pp. 105-145
- Bushnell, D.¹ Rankin, C.C.² Riks, E.³

21
- 0027148268
- Postbuckling response of laminated plates under uniaxial compression
- (1993) Int J Non-Linear Mech , vol.28 , Issue.1 , pp. 95-115
- Shin, D.K.¹ Griffin O.H., Jr.² Gürdal, Z.³

22
- 0004106558
- New York: McGraw-Hill
- (1975) Mechanics of composite materials
- Jones, R.M.¹

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.