Nondimensional parameters for geometric nonlinear effects in pressurized cylinders with axial cracks

Journal of Applied Mechanics, Transactions ASME

Volumn 64, Issue 2, 1997, Pages 401-407

  Budiman, H T ^a   Lagace, P A ^a  

^a Massachusetts Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; COMPUTER SOFTWARE; CRACKS; DYNAMIC RESPONSE; FINITE ELEMENT METHOD; PARAMETER ESTIMATION; STRESS INTENSITY FACTORS;

GEOMETRIC NONLINEAR EFFECTS; SOFTWARE PACKAGE STAGS;

CYLINDERS (SHAPES);

EID: 0031162952     PISSN: 00218936     EISSN: 15289036     Source Type: Journal    
DOI: 10.1115/1.2787322     Document Type: Article

References (28)

1. Ansell, H., 1988, “Bulging of Cracked Pressurized Aircraft Structure,” Ph.D. thesis, Institute of Technology, Department of Mechanical Engineering, Linköping Institute of Technology, Sweden.
2. Brogan, F. A., Rankin, C. C., and Cabiness, H. D., 1994, STAGS User Manual, LMSC P032594, Lockheed Palo Alto Research Laboratory.
3. Budiman, H. T., 1996, “Mechanisms of Damage Tolerance and Arrest in Pressurized Composite Cylinders,” Ph.D. thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA.
4. Chen, D., and Schijve, J., 1991, “Bulging of Fatigue Cracks in a Pressurized Aircraft Fuselage,” Aeronautical Fatigue: Key to Safety and Structural Integrity, A. Kobayashi, ed., Proceeding of the 16th Symposium of the International Committee on Aeronautical Fatigue, Tokyo, Japan, pp. 277-316.
5. Copley, L. G., and Sanders, J. L., 1969, “A Longitudinal Crack in Cylindrical Shell under Internal Pressure,” International Journal of Fracture Mechanics, Vol. 5, No. 2, pp. 117-131.
6. Erdogan, F., and Kibler, J. J., 1969, “Cylindrical and Spherical Shells with Cracks,” International Journal of Fracture Mechanics, Vol. 5, No. 3, pp. 229-237.
7. Flugge, W., 1952, “Stress Problems in Pressurized Cabins,” NACA TN 2612
8. Folias, E. S., 1965, “An Axial Crack in Pressurized Cylindrical Shells,” International Journal of Fracture Mechanics, Vol. 1, No. 2, pp. 104-113.
9. Folias, E. S, 1969, “On the Effects of Initial Curvature on Cracked Flat Sheets,” International Journal of Fracture Mechanics, Vol. 5, No. 4, pp. 327-346.
10. Folias, E. S., 1974a, “Fracture in Pressure Vessels,” Thin Shell Structures: Theory, Experiment, and Design, Y, C. Fung, and E. E. Sechler, eds., Prenlice-Hall, Englewood Cliffs, NJ, pp. 483-518.
11. Folias, E. S., 1974b, “On the Predictions of Catastrophic Failures in Pressurized Vessels,” Prospects of Fracture Mechanics, G. C. Sih, H. C. van Elst, D. Broek, eds., Noordhoff International, Leyden, pp. 405-418.
12. Folias, E. S., 1977, “Asymptotic Approximations to Crack Problems in Shells,” Mechanics of Fracture—Plates and Shells with Cracks, G, C. Sih, ed., Noordhoff International, Leyden, pp. 117-160.
13. Graves, M. J., and Lagace, P. A., 1985, “Damage Tolerance of Composite Cylinders,” Composite Structures, Vol. 4, No. 1, pp. 75-91.
14. Moran, B., and Shih, C. F., 1987, “Crack Tip and Associated Domain Integrals from Momentum and Energy Balance,” Engineering Fracture Mechanics, Vol. 27, pp. 615-641.
15. Niu, C. Y. M., 1988, Airframe Structural Design, Conmilit Press, Ltd.
16. Potyondy, D. O., Wawrzynek, P. A., Ingraffea, A. R., 1995, '‘Discrete Crack Growth Analysis Methodology for Through-Cracks in Pressurized Fuselage Structures,” International Journal for Numerical Methods in Engineering, Vol. 38, No. 10, pp. 1611-1633.
17. Press, W. H., Flannery, B. P., Teukolsky, S. A., and Vetterling, W. T., 1990, Numerical Recipes: The Art of Scientific Computing, Cambridge University Press, New York, pp. 86-89.
18. Ranniger, C. U., Lagacc, P. A., and Graves, M. J., 1995, “Damage Tolerance and Arrest Characteristics of Pressurized Graphite/Epoxy Tape Cylinders,” Composite Materials: Fatigue and Fracture—Fifth Volume, ASTM STP 1230, ASTM, Philadelphia, PA, pp. 407-426.
19. Rankin, C. C., Brogan, F. A., and Riks, E., 1993, “Some Computational Tools for the Analysis of Through Cracks in Stiffened Fuselage Shells,” Computational Mechanics, Vol. 13, pp. 143-156.
20. Rice, J. R., 1972, “Mathematical Analysis in the Mechanics of Fracture,” Fracture, Vol. 2, H. Leibowitz, ed., Academic Press, New York.
21. Riks, E., and den Rijer, P. J., 1987a, “A Finite Element Analysis of Cracks in a Thin Wall Circular Cylinder under Internal Pressure,” NLR TR 87021 U, National Aerospace Laboratory, The Netherlands.
22. Riks, E., 1987b, “Bulging Cracks in Pressurized Fuselages: a Numerical Study,” NLR MP 87058 U, National Aerospace Laboratory, The Netherlands.
23. Riks, E., Brogan, F. A., and Rankin, C. C., 1989, “Bulging Cracks in Pressurized Fuselage: A Procedure for Computation,” Analytical and Computational Models of Shells, A. K. Noor, T. Belytschko, and J. Simo, eds., pp. 483-507
24. Sanders, J. L., Jr., 1963, “Nonlinear Theories for Thin Shells,” Quarterly for Applied Mathematics, Vol. 21, pp. 21-36.
25. Sanders, J. L., Jr., 1982, “Circumferential Through-Cracks in Cylindrical Shells under Tension,” ASME Journal of Applied Mechanics, Vol. 49, pp. 103-107.
26. Swift, T., 1987, “Damage Tolerance in Pressurized Fuselages,” New Materials and Fatigue Resistant Aircraft Design, D. L. Simpson, ed., Proceedings of the 14th Symposium of the International Committee on Aeronautical Fatigue, Ottawa, Canada, pp. 1-77.
27. Viz, M. J., Potyondy, D., Zehnder, A., Rankin, C. C., and Riks, E., 1995, “Computation of Membrane and Bending Stress Intensity Factors for Thin, Cracked Plates,” International Journal of Fracture, Vol. 72, No. 1, pp. 21-38.
28. Yamaki, N., 1984, Elastic Stability of Circular Cylindrical Shells (North Holland Series in Applied Mathematics and Mechanics) Vol. 27, E. Becker, B. Budiansky, W. T. Koiter, and H. A. Lauwerier, eds., North Holland, Amsterdam.