Residual strength analyses of stiffened and unstiffened panels-Part II: Wide panels

Engineering Fracture Mechanics

Volumn 70, Issue 3-4, 2003, Pages 509-524

  Seshadri, B R ^a   Newman Jr , J C ^b   Dawicke, D S ^c  

^a OLD DOMINION UNIVERSITY   (United States)

^b MISSISSIPPI STATE UNIVERSITY   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Crack tip opening angle (CTOA); Elastic plastic finite element analysis; Plane strain core; Wide stiffened panels

Indexed keywords

CRACK PROPAGATION; STRENGTH OF MATERIALS; STRUCTURAL PANELS;

STIFFENERS;

FRACTURE MECHANICS;

CRACK INITIATION; CRACK TIP; PLATE; RESIDUAL STRENGTH;

EID: 0037290691     PISSN: 00137944     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0013-7944(02)00134-0     Document Type: Article

References (23)

1. Damage tolerance in pressurized fuselages
2. Performance of fuselage pressure structure
3. Structural integrity of future aging airplanes
4. Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure
5. Measurement and analysis of critical CTOA for thin-sheet aluminum alloy materials
6. Fracture analysis of stiffened panels under biaxial loading with widespread cracking
7. Three-dimensional CTOA and constraint effects during stable tearing in a thin-sheet material
8. Analyses of buckling and stable tearing in thin-sheet materials
9. Residual strength predictions with crack bulging
10. Computational schemes for integrity analyses of fuselage panels in aging airplanes
11. Residual strength pressure tests and nonlinear analyses of stringer- and frame- stiffened aluminum fuselage panels with longitudinal cracks
12. Fracture analysis of FAA/NASA wide stiffened panels
13. Residual strength analyses of riveted lap-splice joints
14. Fracture simulation of riveted lap-splice joints with a stringer
15. An elastic-plastic finite-element analysis of the J-resistance curve using a CTOD criterion
16. Residual strength predictions for multiple-site damage cracking using a CTOA criterion
17. A fracture criterion for widespread cracking in thin-sheet aluminum alloys