Nonlinear response and residual strength of damaged stiffened shells subjected to combined loads
By: James H. Starnes, Jr. ... [et al.].
Contributors: Starnes, James H.; United States. National Aeronautics and Space Administration.
Series: NASA-TM -- 111889.; NASA technical memorandum -- 111889.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Crack propagation.; Stress intensity factors.; Fuselages.; Shells (Dtructural forms); Residual strength.; Reinforced shells.; Stress distribution.; Finite element method.; Structural analysis.
Notes: Shipping list no.: 97-0681-M.

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