Section 5.0. Analysis Of Damage Growth
The airplane damage tolerance design requirements of JSSG-2006
specify that cracks shall be assumed to exist in all primary aircraft
structure. These cracks shall not grow
to a size to cause loss of the aircraft at a specified load within a specified
period. Showing compliance with these
requirements implies that the rate of growth of the assumed flaws must be
predicted. This section covers basic
crack growth terms, variable amplitude loading, retardation, stress sequence
development, small crack behavior, and crack growth predictions.