The prediction of notch and crack strength under static or fatigue loading.
Fatigue and static strength notch factors in metal parts, using tensile properties and size effect
SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Fatigue and static strength notch factors in metal parts, using tensile properties and size effect
Crack initiation and propagation in notched fatigue specimens of annealed steel and aluminum
Prediction of notch and crack strength under static or fatigue loading
Fatigue and static notch strength analysis of low alloy steels and aluminum and titanium alloys at temperatures from cryogenic to moderately elevated
Cyclic plastic stresses at notch roots of aluminum alloy sheets under repeated tension and reversed loading
Fracture mechanics and notch analysis comparison
Effects of cold rolling on notched and unnotched tensile properties of type 310 stainless steel
Low temperature notch toughness of cryoformed pressure vessels using 301-type stainless steel modifications
Stress-number of cycles characteristics determined for notched aluminum alloy, 7075-T6, specimens, based on fatigue test and mechanical properties
Load cycle prediction for crack initiation and propagation in notched fatigue specimens
Cyclic plastic stresses at notch roots in aluminum alloy sheet specimens under constant- amplitude repeated tension and reversed loading
Stability of infinite plate weakened by hole with sharp notches
Effect of mechanically drilled hole distribution on notch strength of iron alloys
Low cycle fatigue of notched steel and aluminum alloy specimens by consideration of crack initiation and propagation
Cycles required to start crack, and cycles for crack propagation to failure estimated for notched specimen
The validity of the Tada stress intensity factor (K Tada ) for pinned-ends single edge notch tension [SEN(T)] specimens is assessed via a combined experimental-modeling approach. Analysis of fatigue crack growth rate reductions during constant-∆K Tada loading demonstrates that specific combinations of alloy stiffness, geometry, and loading result in the true K deviating below K Tada . Geometrically non-linear, 3-dimensional finite element calculations confirm mild-to-strong influences of these parameters, which are not captured by K Tada . Most existing pinned SEN(T) data are found to use parameters where KTada is not significantly reduced, but the present results underscore the need for a more broadly applicable K solution.
Influence of sheet thickness on sharp-edge-notch properties of a beta titanium alloy at room and low temperatures
Acoustic detection of crack initiation in sharply notched specimens of high strength alloys