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Notch fatigue

Table 7.1 Summary of the parameters of fatigue curves and fatigue notch factors for [0/90] woven glass/polyester tubes under pulsating tension—torsion loading [38]... Table 7.1 Summary of the parameters of fatigue curves and fatigue notch factors for [0/90] woven glass/polyester tubes under pulsating tension—torsion loading [38]...
Fujii T, Shina T, Okubo K. Fatigue notch sensitivity of glass woven fabric composite having a circular hole under tension/torsion biaxial loading. J Compos Mater 1994 28(3) 234-51. [Pg.186]

Ratio of the maximum stress in the region of a notch, or another stress raiser, to the nominal corresponding stress. SCF is a theoretical indication of the effect of stress concentration on mechanical behavior. Since it does not take into account the stress relief due to plastic deformation, its value is usually larger than the empirical fatigue notch factor or strength reducing ratio. External or internal cracks in a plastic caused by imposed stresses. [Pg.2267]

Fatigue notch factor The ratio of the fatigue strength of a specimen with no site of stress concentration (notch) to that of a duplicate specimen having a notch. [Pg.395]

Leis, B.N., Gowda, C.V.B., Topper, T.H. Cyclic inelastic deformation and the fatigue notch factor. Cyclic stress-strain behavior—analysis, experimentation and failure prediction. Am. Soc. Test. Mater., ASTM STP 519, 133-159 (1973)... [Pg.364]

Marry, R.W., Dolan, T.J. The influence of grain size on fatigue notch sensitivity. Proc. ASTM 53, 789 (1953)... [Pg.402]

Mann, J.Y. The fatigue notch sensitivity of annealed copper. Proc. ASTM 60, 602 (1956)... [Pg.402]

Shear Horizontal (SH) waves generated by Electromagnetic Acoustic Transducer (EMAT) have been used for sizing fatigue cracks and machined notches in steels by Time-of-Flight Diffraction (TOED) method. The used EMATs have been Phased Array-Probes and have been operated by State-of-the-art PC based phased array systems. Test and system parameters have been optimised to maximise defect detection and signal processing methods have been applied to improve accuracy in the transit time measurements. [Pg.721]

These values are determined by experiment. It is, however, by no means a trivial task to measure the lamina compressive and shear strengths (52,53). Also the failure of the first ply of a laminate does not necessarily coincide with the maximum load that the laminate can sustain. In many practical composite laminates first-ply failure may be accompanied by a very small reduction in the laminate stiffness. Local ply-level failures can reduce the stress-raising effects of notches and enhance fatigue performance (54). [Pg.14]

General description. In incomplete fusion, complete melting and fusion between the base metal and the weld metal or between individual weld beads does not occur (Fig. 15.8). Incomplete fusion that produces crevices or notches at surfaces can combine with environmental factors to induce corrosion fatigue (Chap. 10), stress-corrosion cracking (Chap. 9), or crevice corrosion (Chap. 2). See Fig. 15.9. [Pg.333]

The data presented in Figure 19.7 were obtained on a Sonntag-Universal machine which flexes a beam in tension and compression. Whereas the acetal resin was subjected to stresses at 1800 cycles per minute at 75°F and at 100% RH, the nylons were cycled at only 1200 cycles per minute and had a moisture content of 2.5%. The polyethylene sample was also flexed at 1200 cycles per minute. Whilst the moisture content has not been found to be a significant factor it has been observed that the geometry of the test piece and, in particular, the presence of notches has a profound effect on the fatigue endurance limit. [Pg.540]

The recommended maximum design stress in tension is one-quarter the ultimate tensile strength (for cast irons a value up to 185 N/mm (12 tonf/ in. )). The fatigue strength is one-half the tensile strength. Notched... [Pg.55]

T. Hoshide, K. Kusuura. Life prediction by simulation of crack growth in notched components with different microstructures and under multiaxial fatigue. Fatigue Fract Eng Mater Struct 27 201, 1998. [Pg.926]

Check slip areas for longitudinal and transverse cracks and sharp notches. Check tool Joints for wear, galls, nicks, washes, fins, fatigue cracks at root of threads, or other items that would affect the pressure holding capacity or stability of the Joint. [Pg.765]


See other pages where Notch fatigue is mentioned: [Pg.143]    [Pg.270]    [Pg.168]    [Pg.189]    [Pg.582]    [Pg.8293]    [Pg.375]    [Pg.376]    [Pg.493]    [Pg.495]    [Pg.374]    [Pg.404]    [Pg.143]    [Pg.270]    [Pg.168]    [Pg.189]    [Pg.582]    [Pg.8293]    [Pg.375]    [Pg.376]    [Pg.493]    [Pg.495]    [Pg.374]    [Pg.404]    [Pg.722]    [Pg.725]    [Pg.728]    [Pg.114]    [Pg.545]    [Pg.89]    [Pg.153]    [Pg.154]    [Pg.269]    [Pg.283]    [Pg.465]    [Pg.953]    [Pg.153]    [Pg.69]    [Pg.70]    [Pg.253]    [Pg.253]    [Pg.56]   
See also in sourсe #XX -- [ Pg.375 , Pg.376 , Pg.377 , Pg.378 , Pg.379 , Pg.380 , Pg.381 ]




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Notch

Notched

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