On the determination of crack opening loads
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Abstract
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Research context
OpenAlex topics: Fatigue and fracture mechanics · Material Properties and Failure Mechanisms · Engineering Diagnostics and Reliability
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References (5)
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1. W. Elber, Damage Tolerance in Aircraft Structures,, STP 486, American Society for Testing and Materials, Philadelphia (1971) 230–242.10.1520/STP26680S ↗
2. H. Fuhring, Berechnung von elastisch-plastischen Beanspruchungsa-bläufen in Dugdale-Risscheiben mit Rissuferkontakt auf der Grundlage nichtlinearer Schwingbruchmechanik, Report of the ISS, TH Darmstadt, (in preparation).
3. V. Bachmann and D. Munz, International Journal of Fracture 11 (1975) 713–716; 12 (1976) 167–168.10.1007/BF00116381 ↗
4. T. T. Shih and R. P. Wei, Engineering Fracture Mechanics 6 (1974) 19–32.10.1016/0013-7944(74)90044-7 ↗
5. J. C. Newman, Jr., A Finite Element Analysis of Fatigue Crack Closure, NASA TMX-72005, Washington (1974).