Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure
By: C.E. Harris ... [et al.].
Contributors: Harris, Charles E., 1950-; Langley Research Center.
Series: NASA technical memorandum -- 110293.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1996
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Subjects: Fuselages; Residual strength; Crack initiation; Crack propagation; Fatigue (Materials); Computer programs
Notes: Shipping list no.: 98-0613-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.