When a fatigue crack is discovered in an engineering component, some e
xpeditious temporary repair may be needed before more thorough treatme
nt is available. Conventional repair methods, such as grinding removal
of the crack and stop drilling, are often employed. In this work, the
method of drilling crack-flank holes near to but not at the crack tip
has been studied. It was found that retardation still occurred. Moreo
ver, if the holes were drilled a small distance ahead of the tip, the
crack was likely to grow into the hole, achieving a considerable amoun
t of life extension. The effects of inducing artificial crack closure
by infiltrating epoxy resin, alumina powder and a mixture of both have
also been investigated. These were compared with the effect of overlo
ad-induced retardation. In all the methods studied, different degrees
of crack growth retardation have been achieved, and they have the pote
ntial to be developed into practical fatigue crack repair methods. Cop
yright (C) 1996 Elsevier Science Limited.