Fatigue life methodology for tapered composite flexbeam laminates
By: Gretchen B. Murri, T. Kevin O'Brien, Carl Q. Rousseau.
Contributors: O'Brien, T. Kevin.; Rousseau, Carl Q.; United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA-CR-204524.; NASA contractor report -- NASA CR-204524.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1997
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Fatigue life.; Finite element method.; Laminates.; Delaminating.; Strain energy release rate.; Cyclic loads.; Glass fiber reinforced plastics.; Epoxy matrix composites.; Fatigue tests.
Notes: Shipping list no.: 98-0933-M.

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