Accession Number : ADA953044

Title :   Fatigue Crack Retardation Following a Single Overload.

Descriptive Note : Technical memo.,

Corporate Author : AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH

Personal Author(s) : Gray,T. D.

Report Date : OCT 1973

Pagination or Media Count : 17

Descriptors :   *Mathematical prediction, Fatigue(Mechanics), Crack propagation, Aluminum, Steel, Titanium alloys, Retardation, Overload, Loads(Forces), Cyclic tests, Mathematical models, Experimental data, Stresses, Yield strength, Formulas(Mathematics)

Subject Categories : Metallurgy and Metallography
      Numerical Mathematics
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE