Analyses of buckling and stable tearing in thin-sheet materials

NASA Technical Memorandum

Volumn , Issue 208428, 1998, Pages 1-26

  Seshadri, B R ^a   Newman Jr , J C ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 12944331246     PISSN: 04999320     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (16)

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3. Newman, J. C., Jr., "An Elastic-Plastic Finite-Element Analysis of Crack Initiation, Stable Crack Growth, and Instability," Fracture Mechanics - Fifteenth Symposium, ASTM STP 833, R. J. Sanford, Ed., American Society for Testing and Materials, Philadelphia, PA, 1984, pp. 93-117.
4. Newman, J. C. Jr., Dawicke, D. S. and Bigelow, C.A., "Finite-Element Analyses and Fracture Simulation in Thin-Sheet Aluminum Alloys", Durability of Metal Aircraft Structures, S. N. Atluri et al., Eds., Atlanta, Georgia, 1992, pp. 167-186.
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7. Forman, R. G., "Experimental Program to Determine Effect of Crack Buckling and Specimen Dimensions on Fracture Toughness of Thin Materials", Technical Report AFFDL-TR-65-146, January 1966.
8. Brogan, F. A., Rankin, C. C. and Cabiness, H. D., "STAGS Users Manual", Lockheed Palo Alto Research Laboratory, Report LMSC P032594, 1994.
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10. Dawicke, D. S. and Newman, J. C., Jr., "Residual Strength Predictions for Multiple-Site Damage Cracking using a CTOA Criterion," Fatigue and Fracture Mechanics: 29th Volume, ASTM STP 1332, T. L. Panontin and S. D. Sheppard, Eds., American Society for Testing and Materials, Philadelphia, PA, 1998.
11. Dawicke, D. S., "Fracture Tests on 0.09 Inch Thick 2024-T3 Aluminum Alloy", NASA TM 112869 , National Aeronautics and Space Administration, 1997.
12. Newman, J. C., Jr., Booth, B. C. and Shivakumar, K. N., "An Elastic-Plastic Finite-Element Analysis of the J-Resistance Curve using a CTOD Criterion", Fracture Mechanics: Eighteenth Symposium, ASTM STP 945, D. T. Read and R. P. Reed, Eds., American Society for Testing and Materials, Philadelphia, PA, 1988, pp. 665-685.
13. Newman, J. C., Jr.; Dawicke, D. S.; Sutton, M. A. and Bigelow, C. A., "A Fracture Criterion for Widespread Cracking in Thin-Sheet Aluminum Alloys", Durability and Structural Integrity of Airframes, Vol. I, A. F. Blom, Ed., 1993, pp. 443-468.
14. Swift, T., "Damage Tolerance in Pressurized Fuselages," New Materials and Fatigue Resistant Aircraft Design, 14th Symposium of the International Committee on Aeronautical Fatigue (ICAF), Ottawa, Canada, June 1987.
15. Newman, J. C. Jr. and Dawicke, D. S., "Fracture Analysis of Stiffened Panels under Biaxial Loading with Widespread Cracking", Widespread Fatigue Damage in Military Aircraft, AGARD CP-568, 1995, pp. 3.1-3.16.
16. Broek, D., Thomson, D. and Jeong, D. Y., "Testing and Analysis of Flat and Curved Panels with Multiple Cracks," NASA Conference Publication 3274, Part II, September 1994, pp. 963-984.