Use of finite element computer programs in fracture mechanics
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OpenAlex topics: High-Velocity Impact and Material Behavior · Electromagnetic Launch and Propulsion Technology · Rocket and propulsion systems research
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References (12)
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1. A. A. Griffith, The Phenomena of Rupture and Flow in Solids, Philosophical Transactions, London: Royal Society, Series A, Vol. 221, (1920) 163–198.
2. M. L. Williams, Initiation and Growth of Viscoelastic Fracture, International Journal of Fracture Mechanics, 1 (1965) 4.10.1007/BF03545558 ↗
3. G. R. Irwin, Fracture, Encyclopedia of Physics, Springer, Berlin, VI (1958) 551–590.
4. TWR-3532 Final Report Grain Stress Analysis, SLIM Program — Task 2, Vol. I, Thiokol Chemical Corporation November 1969.
5. Determination of Optimum Length of End Release for Case Bonded Solid Propellant Rocket Motors, AFRPLTR-67-72, March 1967.
6. S. R. Swanson, Crack Propagation in Solid Rocket Propellant Grains Under Ignition Loading, M.S. Thesis, Department of Mechanical Engineering, University of Utah, June 1968.
7. S. K. Chan, I. S. Tuba and W. K. Wilson, On the Finite Element Method in Linear Fracture Mechanics, Scientific Paper 68–107-FMPWR-P1, Westinghouse Research Laboratories, Pittsburgh, Pa., 2 April 1968.
8. S. J. Bennett, G. P. Anderson and M. L. Williams, The Time Dependence of Surface Energy in Cohesive Fracture, Journal of Applied Polymer Science14, 735 (1970).10.1002/app.1970.070140317 ↗
9. P. C. Paris and G. C. Sih, Stress Analysis of Cracks, ASTM Special Technical Publication No. 381, June 1964.
10. O. L. Bowie, Analysis of an Infinite Plate Containing Radial Cracks Originating at the Boundary of an Internal Circular Hole, Journal of Mathematical Physics, (1956) 60–70.10.1002/sapm195635160 ↗
11. J. R. Rice, A Path Independent Integral and the Approximate Analysis of Strain Concentration by Notches and Cracks, Journal of Applied Mechanics, Transactions of the ASME Series E 35, 2, 379–386, June 1968.10.1115/1.3601206 ↗
12. M. L. Williams, P. J. Blatz and R. A. Schapery, Fundamental Studies Relating to Systems Analysis of Solid Propellants, GALCIT SM 61–5 Guggenheim Aeronautical Laboratory, California Institute of Tech., Pasadena, California, 1961.10.21236/AD0256905 ↗