SCOPUS 정보 검색 플랫폼

Composites - Part A: Applied Science and Manufacturing

Volumn 32, Issue 6, 2001, Pages 859-870

Compressive response of notched glass-fiber epoxy/honeycomb sandwich panels

(2) Toribio, M G a Spearing, S M a

a Massachusetts Institute of Technology (United States)

Author keywords

Damage mechanics; Glass fibres; Transverse cracking

Indexed keywords

COMPRESSION TESTING; COMPRESSIVE STRENGTH; CRACK PROPAGATION; EPOXY RESINS; FAILURE ANALYSIS; MATHEMATICAL MODELS; SANDWICH STRUCTURES; STRUCTURAL PANELS;

TRANSVERSE CRACKING;

GLASS FIBER REINFORCED PLASTICS;

EID: 0035372422 PISSN: 1359835X EISSN: None Source Type: Journal
DOI: 10.1016/S1359-835X(00)00150-0 Document Type: Article

Times cited : (21)

References (27)

1
- 0005424312
- Airframers stress durability in composites
- (1995) Aviat Week Space Technol , vol.142 , pp. 60-61
- Smith, B.A.¹

2
- 0033098790
- Eurofighter parts designed for composites
- (1999) Adv Mater Process , vol.155 , pp. 45-46
- Williams, A.¹ Birchall, B.² Rishton, J.³

3
- 0028026488
- Flight service evaluation of composite helicopter components
- (1994) J Am Helicopter Soc , vol.39 , pp. 31-40
- Mardoian, G.H.¹ Ezzo, M.B.²

4
- 0031621132
- Damage tolerance evaluation of composite honeycomb structures
- SAMPE, Covina, CA, USA
- (1998) International SAMPE Symposium and Exhibition (Proceedings) , vol.43 , pp. 376-386
- Abbott, R.¹

5
- 0003485591
- PhD thesis, Massachusetts Institute of Technology, TELAC Report 94-5
- (1994) Impact resistance and damage tolerance of composite sandwich panels , vol.94
- Tsang, P.H.W.¹

6
- 0004037922
- SM thesis, Massachusetts Institute of Technology, TELAC Report 89-3
- (1989) Damage resistance and damage tolerance of thin composite facesheet honeycomb panels
- Lie, S.C.¹

7
- 0025434601
- Evaluation of advanced sandwich structure designed for improved durability and damage tolerance
- Washington, DC
- (1990) Forty-sixth Annual Forum of the American Helicopter Society , pp. 825-831
- Llorente, S.¹ Weems, D.² Fay, R.³

8
- 0031654109
- Low velocity impact response of resin infusion molded foam filled honeycomb sandwich composites
- (1998) J Reinforced Plast Compos , vol.17 , pp. 819-849
- Vaidya, U.K.¹ Kamath, M.V.² Mahfuz, H.³ Jeelani, S.⁴

9
- 0031358847
- Low-velocity impact damage initiation in graphite/epoxy/Nomex honeycomb sandwich plates
- (1997) Compos Sci Technol , vol.57 , pp. 1581-1598
- Herup, E.J.¹ Palazotto, A.N.²

10
- 0344672594
- Localized damage response of composite sandwich plates
- (1999) Compos Part B: Engng , vol.30 , pp. 157-165
- Turk, M.H.¹ Hoo Fatt, M.S.²

11
- 0028467862
- Microbuckle propagation in carbon fibre-epoxy composites
- (1994) Acta Metall Mater , vol.42 , Issue.7 , pp. 2219-2231
- Sutcliffe, M.P.F.¹ Fleck, N.A.²

12
- 0030190160
- Microbuckle propagation in a unidirectional carbon fibre-epoxy matrix composite
- (1996) Acta Mater , vol.44 , pp. 2581-2590
- Sivashanker, S.¹ Fleck, N.A.² Sutcliffe, M.P.F.³

13
- 4243805419
- MS thesis, Texas A&M University
- (1987) Micromechanics of compression failures in open hole composite laminates
- Guynn, E.G.¹

14
- 85165995771
- Micromechanics of compression failures in open hole composite laminates
- Composite Materials: Fatigue and Fracture, ASTM
- (1989) ASTM STP 1012 , vol.2 , pp. 118-136
- Guynn, E.G.¹ Bradley, W.L.² Elber, W.³

15
- 84970392984
- Measurements of the stress supported by the crush zone in open hole composite laminates loaded in compression
- (1989) J Reinforced Plast Compos , vol.8 , pp. 133-149
- Guynn, E.G.¹ Bradley, W.L.²

16
- 0024666039
- A detailed investigation of the micromechanisms of compressive failure in open-hole composite laminates
- (1989) J Compos Mater , vol.23 , pp. 479-504
- Guynn, E.G.¹ Bradley, W.L.²

17
- 0003592729
- PhD thesis, Cambridge University
- (1989) Compressive failure of notched carbon fibre-epoxy panels
- Soutis, C.¹

18
- 84972758412
- Static compression failure of carbon fibre T800/924C composite plate with a single hole
- (1990) J Compos Mater , vol.24 , pp. 536-558
- Soutis, C.¹ Fleck, N.A.²

19
- 0029331914
- Compressive failure of laminated and woven composites
- (1995) J Compos Technol Res , vol.17 , pp. 212-220
- Fleck, N.A.¹ Jelf, P.M.² Curtis, P.T.³

20
- 0026258816
- Failure prediction technique for compression loaded carbon fibre-epoxy laminate with open holes
- (1991) J Compos Mater , vol.25 , pp. 1476-1498
- Soutis, C.¹ Fleck, N.A.² Smith, P.A.³

21
- 0032090518
- Damage growth in carbon fibre-PEEK unidirectional composites under compression
- (1998) Mater Sci Engng A - Struct Mater Properties Microstruct Process , vol.249 , pp. 259-276
- Sivashanker, S.¹

22
- 50549180512
- Yielding of steel sheets containing slits
- (1960) J Mec Phys Solids , pp. 118-136
- Dugdale, D.S.¹

23
- 0035339158
- Damage modeling of notched graphite/epoxy sandwich panels in compression
- in press
- (2001) Appl Compos Mater
- Mirazo, J.M.¹ Spearing, S.M.²

24
- 0002306579
- A nonlinear fracture mechanics approach to the growth of small cracks
- France
- (1982) AGARD Conference Proceedings , vol.328 , pp. 616-626
- Newman, J.C.J.¹

25
- 3142729120
- Massachusetts Institute of Technology, TELAC Report 99-6, MIT, June
- (1999) Compressive response of notched composite - honeycomb sandwich panels
- Toribio, M.G.¹

26
- 0005414243
- NASA CP 2142, NASA
- (1980) Failure prediction techniques for compression loaded composite laminates with holes
- Mikulas, M.M.¹

27
- 0021786837
- Notched strength of composite laminates: Predictions and experiments - A review
- (1985) J Reinforced Plast Compos , vol.4 , pp. 3-159
- Awerbuch, J.¹ Madhukar, M.S.²

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.