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STRESS CONCENTRATION AT NOTCHES. One of the fundamental issues of designing a resistant structure (specially in “design against fracture” and “design against fatigue”) is the consideration of stress concentrations.
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STRESS CONCENTRATION AT NOTCHES One of the fundamental issues of designing a resistant structure (specially in “design against fracture” and “design against fatigue”) is the consideration of stress concentrations Stress concentration at geometrical notches are always present in a real structure Notches introduce inhomogeneous stress distribution with a stress concentration at the root of the notch Stress concentration factor: Ktis referred as the theoretical stress concentration factor: it is based in the assumption of linear elastic material behavior Kt describes the severity of the notch and depends on the geometry of the notch configuration (shape factor of the notch)
Common examples of stress concentration • Gear teeth • Shaft keyway • Bolt threads • Shaft shoulder • Riveted or bolted joint • Welded joint
DEFINITIONS: For the previous example: therefore: In general Kt is the preferred factor to indicate stress concentration following the definitions of R.E. Peterson in Stress Concentration Factors, John Wiley & Sons, New York (1974)
THE “MODEL” STRESS CONCENTRATION CASE: the circular hole in an infinite sheet S r r0 q S Along the edge of the circular hole: compression at q = 0 • q for sqq = 0 ?
Circular Hole: STRESS PROFILES • We are interested in evaluating: • Situation for compressive remote stress (–S): presence of tensile stress! • Gradient of Stress in the direction normal to the edge of the hole at the location of speak: strong gradient • Gradient of Stress along the edge of the hole at the location of speak : much less stronger as along the normal • Volume of material subjected to high Stress around the root of the notch: larger for larger notches! (significant to understand notch size effects on fatigue)
S S Slow decrease of the stress along the edge compared with the decrease from the edge at the location of speak
Geometrically similar specimens have the same Kt but different stress gradients Larger specimens have larger volumes and larger notch surface areas of highly stressed material Important !!!: Notch Size Effects in Fatigue
The elliptical hole in an infinite sheet S S use large radii to reduce stress concentration !
Stress Concentration for an elliptical hole under biaxial loading: * For the case of a thin walled pressure vessel under pressureb = 0.5 and for the case of a circular hole (a = b): lower than 3 S for uniaxial loading b: biaxiality ratio * Same case but elliptical hole with b/a = 2: compare with the square hole (dashed line) with rounded corners with r 10% of hole width: Kt = 4.04 for b = 0.5 lower than 3 S for uniaxial loading (actually, sqq = 1.5 S along the edge of the hole)
Stress Concentration for a circular hole in a plate under pure shear: ! Fatigue cracks growing from holes in a shaft subjected to cyclic torsion
Stress concentration factors for a shaft with a grove subjected to: axial load torsion
Edge notches and Corrosion Pits Corosion pits at the material surface of an Al-alloy. Pit depth = 0.15 mm. Equivalent shape gives very high Kt values
SUPERPOSITION OF NOTCHES: If a relativelly small notch is added to the root of the main notch superposition of notches: This overestimates Kt because the small notch is not embedded in an homogeneous stress field of magnitude Kt1
Further Examples: Lug with small lubrication hole to the lug hole Cross section of a fatigue crack at a sharp corner