PSI - Issue 75
Andrew Halfpenny et al. / Procedia Structural Integrity 75 (2025) 219–233 Author name / Structural Integrity Procedia (2025)
233 15
Brussat, T. R., 1974. Rapid Calculation of Fatigue Crack Growth by Integration. Fracture Toughness and Slow-Stable Cracking, 298 – 311. Chang, J. B., Engle, R. M., 1984. Improved damage-tolerance analysis methodology. Journal of Aircraft 21(9), 722 – 730. Elber, W., 1971. The Significance of Fatigue Crack Closure. Damage Tolerance in Aircraft Structures, 230 – 242. Forman, R., Kearney, V. E., Engle, R., 1967. Numerical Analysis of Crack Propagation in Cyclic-Loaded Structures. ASME Journal of Basic Engineering 89(3), 459 – 463. Gallagher, J. P., 1974. A generalised development of yield zone models. Air Force Flight Dynamics Laboratory Technical Memorandum 74-28 FBR. Griffith, A. A., 1921. The phenomena of rupture and flow in solids. Philosophical Transactions of the Royal Society of London. Series A, Containing Papers of a Mathematical or Physical Character 221, 163 – 198. Harter, J. A., 2000. Afgrow Users Guide and Technical Manual. Air Vehicles Directorate, 2790 D Street, Ste 504, Air Force Research Laboratory, WPAFB OH 45433-7542, USA. Irwin, G. R., 1958. Fracture. In: Flügge, S. (eds) Elasticity and Plasticity / Elastizität und Plastizität. Handbuch der Physik / Encyclopedia of Physics 3/6, 551 – 590. Springer, Berlin, Heidelberg. Irwin, G. R., 1960. Plastic zone near a crack and fracture toughness. In: 7th Sagamore Ardance Materials Research Conference, Syracuse, Univ. Press. Kitagawa, H., Takahashi, S., 1976. Applicability of Fracture Mechanics to Very Small Cracks or the Cracks in the Early Stage. In: Proceedings of the 2nd International Conference on Mechanical Behaviour of Materials, 627 – 631. Mettu, S. R., Shivakumar, V., Beek, J. M., Yeh, F., Williams, L. C., Forman, R. G., McMahon, J. J., Newman Jr., J. C., 1999. NASGRO 3.0: A software for analyzing aging aircraft. NASA, 1999. Reference Manual for NASGRO version 3. Lyndon B. Johnson Space Center, 2101NASA Road 1, Houston, Texas 77058-3696, USA. nCode, 2003. ICE-Flow Crack Growth Quick Start Guide V2.0. Paris, P., Erdogan, F., 1963. A Critical Analysis of Crack Propagation Laws. Journal of Basic Engineering 85(4), 528 – 534. Press, W. H., Teukolsky, S. A., Vetterling, W. T., Flannery, B. P., 2007. Numerical Recipes in C: The Art of Scientific Computing (3rd ed.). Cambridge University Press. Walker, K., 1970. The Effect of Stress Ratio During Crack Propagation and Fatigue for 2024-T3 and 7075-T6 Aluminum. Effects of Environment and Complex Load History on Fatigue Life, ASTM STP 462. Wheeler, O. E., 1972. Spectrum loading and crack growth. ASME Journal of Basic Engineering 94(1), 181 – 186. Willenborg, J. F., Engle, R. M., Wood, H. A., 1971. A Crack Growth Retardation Model Using an Effective Stress Concept. Air Force Flight Dynamics Laboratory Technical Memorandum 71-1-FBR.
Made with FlippingBook flipbook maker