TourTour Preloaded bolt under dynamic loading
 Metric thread : -
 Initial tensile stress : σi=Fi/At xRp0.2 
 Minimum value of clamping force: Fm kN
 Joint stiffness factor C=kb/(kb+km)
 
ISO 724 tensile stress area At =π/4 d02 ; d0=(d2+d3)/2 mm2
 ultimate tensile strength Rm  MPa
 yield strength Rp0.2 MPa
 initial tensile stress σt = σ't x Rp0.2 MPa
 maximum tensile load F0.2 = Rp0.2 x At kN
 initial preload Fi = σt x At kN
 load fluctuation bolt dFi =F0.2 - Fi kN
 bolt stress fluctuation i = dFi / At MPa
 load fluctuation clamped material dFm=dFi *(1-C )/C kN
 remaining clamping force Fm=Fi -dFm kN
 Total load fluctuation Fb= dFi + dFm kN

Static strength:
The warning about the fatigue strength can be ignored.

Fatigue strength: In infinite life or safe stress designs stresses higher then the endurance limit are avoided and a factor of safety is taken into account. Most rotating and oscillating components must sustain over 10^6 load cycles during service life and thus are to be designed for infinite fatigue life.
 

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