Interaction of multiple cracks are found in mud when drying and crazin
g, thin film varnishes or coatings of aeroengine turbine blades. A two
-dimensional multiple crack interaction model is developed to simulate
the growth of interacting parallel surface cracks. Density and the in
itial distribution of the microcracks are accounted for in analyzing t
he growth of a crack to a pre-determined length. Analytical prediction
s are discussed with reference to experimental observations of fatigue
cracks on coated turbine blades. Introduction of a large density of s
imilar cracks can enhance the fatigue life of structural components.