SCOPUS 정보 검색 플랫폼 - 논문 보기

메뉴 건너뛰기

International Journal of Non-Linear Mechanics

Volumn 37, Issue 4-5, 2002, Pages 833-849

STAGS computational procedure for progressive failure analysis of laminated composite structures

(3) Knight Jr , Norman F a Rankin, Charles C b,c Brogan, Frank A b

a Veridian Systems Division (United States)

b LOCKHEED MARTIN (United States)

c NONE (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; FAILURE ANALYSIS; FINITE ELEMENT METHOD; LAMINATED COMPOSITES;

PROGRESSIVE FAILURE ANALYSIS (PFA);

COMPOSITE STRUCTURES;

EID: 0036604699 PISSN: 00207462 EISSN: None Source Type: Journal
DOI: 10.1016/S0020-7462(01)00101-9 Document Type: Article

Times cited : (24)

References (31)

1
- 0003406221
- Lockheed Martin Missiles and Space Co., Inc., Palo Alto, CA, Report No. LMSC P032594
- (2000) STAGS User Manual - Version 4.0
- Rankin, C.C.¹ Brogan, F.A.² Loden, W.A.³ Cabiness, H.D.⁴

2
- 0007655670
- Lockheed Palo Alto Research Laboratory, Palo Alto, CA, Contract Report No. F318484
- (1991) Computational mechanics testbed (COMET) generic constitutive processor manual
- Hurlbut, B.J.¹ Stehlin, B.P.²

3
- 4244193786
- MS Thesis, Department of Aerospace Engineering, Old Dominion University, Norfolk, VA, Also available as NASA TP-1999-209107, 1999
- (1996) Progressive failure analysis of laminated composite structures
- Sleight, D.W.¹

4
- 0006396563
- Evaluation of a progressive failure analysis methodology for laminated composite structures
- (1997) AIAA Paper , vol.97 , Issue.1187
- Sleight, D.W.¹ Knight N.F., Jr.² Wang, J.T.³

5
- 0007614245
- Final Report to NASA Langley Research Center under GSA Contract No. GS-35F-4503G, Veridian MRJ Technology Solutions, Task 1417
- (2000) Further enhancement of STAGS progressive failure capability
- Knight N.F., Jr.¹

6
- 85067316609
- Controlling progressive failure analyses using artificial viscous damping
- (2001) AIAA Paper , vol.2001 , Issue.1180
- Knight N.F., Jr.¹ Rankin, C.C.² Brogan, F.A.³

7
- 0023420567
- A progressive damage model for laminated composites containing stress concentrations
- (1987) J. Compos. Mater. , vol.21 , pp. 834
- Chang, F.-K.¹ Chang, K.-Y.²

8
- 4244168219
- Ph.D. Dissertation, Department of Civil Engineering, Stanford University
- (1993) Progressive failure analysis of laminated composites subjected to in-plane tensile and shear loads
- Shahid, I.¹

9
- 0027202962
- Non-linear response of composite laminates due to material non-linearity and accumulated damage
- M.W. Hyer (Ed.)
- (1993) Mechanics of Composite Materials: Non-linear Effects , vol.AMD-159 , pp. 319
- Shahid, I.¹ Chang, F.-K.²

10
- 0007654856
- Modeling of failure and response to laminated composites subjected to in-plane loads
- A.K. Noor, C.E. Harris, D.A. Hopkins (Compilers), Computational Methods for Failure Analysis and Life Prediction
- (1993) NASA CP-3230 , pp. 83
- Shahid, I.¹ Chang, F.-K.²

11
- 0000356907
- An accumulative damage model for tensile and shear failures of laminated composite plates
- (1995) J. Compos. Mater. , vol.29 , pp. 926
- Shahid, I.¹ Chang, F.-K.²

12
- 4244168218
- Ph.D. Dissertation, Department of Mechanical Engineering, Stanford University
- (1997) Modeling the in-plane tension failure of composite plates
- Trinh, K.V.¹

13
- 0007620084
- Hibbitt, Karlsson and Sorenson, Inc., Pawtucket, RI
- (1996) ABAQUS/Standard User's Manual, vol III, version 5.6 , vol.3

14
- 0019024701
- Failure criteria for unidirectional fiber composites
- (1980) ASME J. Appl. Mech. , vol.47 , pp. 329
- Hashin, Z.¹

15
- 0014974615
- A general theory of strength for anisotropic materials
- (1971) J. Compos. Mater. , vol.5 , pp. 58
- Tsai, S.W.¹ Wu, E.M.²

16
- 0023538202
- Modeling of damage development in composites using internal variable concepts
- A.S.D. Wang, G.K. Haritos (Eds.), ASME
- (1987) Damage Mechanics in Composites , vol.AD-12 , pp. 11
- Talreja, R.¹

17
- 0023590232
- A thermomechanical constitutive theory for elastic composites with distributed damage - I. Theoretical development
- (1987) Int. J. Solids Struct. , vol.23 , pp. 1301
- Allen, D.H.¹ Harris, C.E.² Groves, S.E.³

18
- 0023532780
- A thermomechanical constitutive theory for elastic composites with distributed damage - II. Application to matrix cracking in composite laminates
- (1987) Int. J. Solids Struct. , vol.23 , pp. 1319
- Allen, D.H.¹ Harris, C.E.² Groves, S.E.³

19
- 0026284347
- A model for the progressive failure of laminated composite structural components
- L. Schwer, J.N. Reddy, A. Mal (Eds.), ASME
- (1991) Enhancing Analysis Techniques for Composite Materials , vol.NDE-10 , pp. 125
- Allen, D.H.¹ Lo, D.C.²

20
- 0029211213
- Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue
- (1995) J. Compos. Mater. , vol.29 , pp. 280
- Coats, T.W.¹ Harris, C.E.²

21
- 0007653502
- Progressive damage analysis of laminated composite (PDALC) - A computational model implemented in the NASA COMET finite element code
- (1996) NASA TM-4724
- Lo, D.C.¹ Coats, T.W.² Harris, C.E.³ Allen, D.H.⁴

22
- 0007611365
- A progressive damage methodology for residual strength predictions of notched composite panels
- (1998) NASA TM-1998-207646
- Coats, T.W.¹ Harris, C.E.²

23
- 0006722873
- On the numerical solution of snapping problems in the theory of elastic stability
- Stanford University, Also available as AFOSR 70-2258TR
- (1970) Report SUDAAR , vol.401
- Riks, E.¹

24
- 4244067787
- Final Report under Contract No. TZ-370444-07LHN, Department of Aeronautics and Astronautics, Stanford University
- (2000) Damage tolerance-based design of bolted composite joints
- Chang, F.-K.¹ Qing, X.² Sun, H.-T.³ Yan, Y.⁴

25
- 0019479471
- Postbuckling and failure characteristics of selected flat rectangular graphite-epoxy plates loaded in compression
- (1981) AIAA Paper , vol.81 , Issue.543
- Starnes J.H., Jr.¹ Rouse, M.²

26
- 0002029948
- LLC: Shear measurement or sheer myth?
- R.B. Bucinell (Ed.), ASTM STP1330
- (1998) Composite Materials: Fatigue and Fracture , vol.7 , pp. 3
- O'Brien, T.K.¹

27
- 0026907759
- Postbuckling response and failure prediction of graphite-epoxy plates loaded in compression
- (1992) AIAA J. , vol.30 , pp. 2106
- Engelstad, S.P.¹ Reddy, J.N.² Knight N.F., Jr.³

28
- 0007614656
- Postbuckling of flat unstiffened graphite-epoxy plates in shear
- (1985) AIAA Paper , vol.85 , Issue.771 CP
- Rouse, M.¹

29
- 0035254336
- Buckling behavior of compression-loaded quasi-isotropic curved panels with a circular cutout
- (2001) Int. J. Solids Struct. , vol.38 , pp. 1495
- Hilburger, M.W.¹ Britt, V.O.² Nemeth, M.P.³

30
- 0007621195
- private communication, March
- (2001)
- Hilburger, M.W.¹

31
- 85067319277
- Progressive failure studies of composite panels with and without cutouts
- (2001) AIAA Paper , vol.2001 , Issue.1182
- Ambur, D.R.¹ Jaunky, N.² Davila, C.G.³ Hilburger, M.W.⁴

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.