The fatigue fracture surfaces of a metallic alloy, and the stress corrosion
fracture surfaces of glass are investigated as a function of crack velocity. It
is shown that in both cases, there are two fracture regimes, which have a well
defined self-affine signature. At high enough length scales, the universal
roughness index 0.78 is recovered. At smaller length scales, the roughness
exponent is close to 0.50. The crossover length ξc separating these two
regimes strongly depends on the material, and exhibits a power-law decrease
with the measured crack velocity ξc∝v−ϕ, with ϕ≃1. The exponents ν and β characterising the dependence of ξc
and v upon the pulling force are shown to be close to ν≃2 and
β≃2.Comment: 4 pages, latex, and 4 encapsulated postscript figure