Experimental Study of Sable Crack Growth in Thin Aluminium Sheet

S. H. Hashemi

Volume 5, Issue 4 , December 2008, , Pages 183-190

Abstract
  Recent failure information from research teams in NASA Langley and others has shown that CTOA based fracture models calibrated on large C(T) and M(T) specimens can be transferred successfully to cracked aircraft fuselage structures for the assessment of their residual strength. A major difficulty that ...  Read More