1-20 of 417 Search Results for

fatigue crack propagation

Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Image
Published: 01 December 2003
Fig. 3 Thermal fatigue failure and conventional fatigue crack propagation fracture during reversed load cycling of acetal. Source: Ref 10 More
Image
Published: 01 June 2008
Fig. 14.15 Fatigue crack propagation. Source: Ref 6 More
Image
Published: 01 December 2003
Fig. 9 Fatigue-crack-propagation behavior. ABS, acrylonitrile-butadiene-styrene; PC, polycarbonate; M-PPE, modified polyphenylene ether More
Image
Published: 01 December 2003
Fig. 7 Specimens employed in fatigue crack propagation studies. (a) Single-edge-notch specimen. (b) Compact-tension specimen More
Image
Published: 01 December 2003
Fig. 11 Comparison of fatigue crack propagation behavior in the Paris regime for several amorphous and semicrystalline polymers. Note enhanced fatigue resistance of the semicrystalline polymers. PC, polycarbonate; PMMA, polymethyl methacrylate; PPO, polypropylene oxide; PVF, polyvinyl formal More
Image
Published: 01 December 2003
Fig. 12 Fatigue crack propagation behavior for a rubber-toughened epoxy. The addition of rubber decreases the slope, m , at high crack growth rates due to toughening mechanisms and retarded crack growth. CTBN, carboxylterminated polybutadiene acrylonitrile rubber; MBS, methacrylate-butadiene More
Image
Published: 01 December 2003
Fig. 8 An S-shaped fatigue crack propagation. K , stress-intensity factor; K c , fracture toughness curve indicating its three characteristic regions. More
Image
Published: 01 December 2003
Fig. 9 Fatigue crack propagation behavior of various polymers. PSU, polysulfone; PMMA, polymethyl methacrylate; PC, polycarbonate; PS, polystyrene; PVC, polyvinyl chloride. Source: Ref 48 More
Image
Published: 01 December 2003
Fig. 10 The rate of fatigue crack propagation of injection-molded glass-reinforced polyvinyl chloride composites containing 10 and 30% glass as a function of the energy release rate, J I . Arrows indicate the critical energy release rate, J Ic , for each. More
Image
Published: 01 December 2003
Fig. 11 Fatigue crack propagation rates ( da / dN ) at 10 Hz as a function of stress-intensity factor range (Δ K ) in low-density polyethylene. da / dN decreases with increasing Δ K . Source: Ref 51 More
Image
Published: 01 September 2008
Fig. 13 Stages I and II of fatigue crack propagation More
Image
Published: 01 November 2012
Fig. 30 Fatigue crack propagation. Source: Ref 17 More
Image
Published: 01 August 2005
Fig. 5.56 Effect of applied stress on fatigue crack propagation More
Image
Published: 01 August 2005
Fig. 5.61 Schematic stress profiles for fatigue crack propagation testing showing the effects of overload/underload with hold time. Source: Ref 5.72 More
Image
Published: 01 August 2005
Fig. 5.68 Influence of testing temperature on fatigue crack propagation exponent for iron-base alloys. Source: Ref 5.83 More
Image
Published: 01 December 1989
Fig. 4.43. Results of 20 experiments showing correlation of fatigue-crack-propagation rates in A533B steel in terms of cyclic J for a variety of specimen configurations ( Ref 168 ). More
Image
Published: 01 December 2000
Fig. 12.29 Fatigue crack propagation data for mill-annealed alpha-beta alloy Ti-6Al-4V showing data scatter. Data are for six heats of mill-annealed Ti-6Al-4V. T-L, transverse-longitudinal More
Image
Published: 01 December 2000
Fig. 12.43 Comparison of room-temperature fatigue crack propagation rate for a Ti-6Al-4V powder metallurgy compact with the scatter bands for wrought ingot metallurgy products of the alloy. I/M, ingot metallurgy; P/M, powder metallurgy More
Image
Published: 01 December 2000
Fig. 12.49 Fatigue crack propagation rates for Ti-5Al-2.5Sn and Ti-6Al-4V alloys in the low-temperature region. NI = normal interstitial content; ELI = extra low interstitial content More
Image
Published: 01 July 1997
Fig. 12 Fatigue crack propagation rates of wrought aluminum alloys. Source: Ref 7 More