Response of composite panels with stiffness gradients due to stiffener terminations and cutouts
By: Damodar R. Ambur ... [et al.].
Contributors: Ambur, Damodar R.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 112845.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1997
Place of publication: [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Composite structures.; Aircraft structures.; Graphite-epoxy composites.; Failure modes.; Finite element method.; Stiffening.
Notes: Shipping list no.: 98-0599-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche. (NASA-TM ; 112845).