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Fatigue crack growth from a circular hole with and without high prior loading

Fatigue crack growth from a circular hole with and without high prior loading - - Washington, D.C. National Aeronautcs ad space Association 1972 - 33 P. - NASA TN D-6899 : 1972 .

ISBN:

Subjects--Topical Terms:

Crack propagation,Stress concentration,Stress intensity factors,High prior loading,Residual stress

Universal Decimal Class. No.: LNASA TN D-6899 : 1972

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