Fracture analysis of stiffened panels under biaxial loading with widespread cracking
By: J.C. Newman, Jr.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 110197.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aluminum alloys.; Axial loads.; Crack propagation.; Crack tips.; Cracking (Fracturing).; Finite element method.; Metal fatigue.; Panels.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0224-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.