Fatigue life methodology for tapered composite flexbeam laminates
By: Gretchen B. Murri and T. Kevin O'Brien, Carl Q. Rousseau.
Contributors: O'Brien, T. Kevin.; Rousseau, Carl Q.; Langley Research Center.
Series: NASA technical memorandum -- 112860.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1997
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Strain energy release rate.; Finite element method.; Laminates.; Delaminating.; Fatigue life.; Fatigue (Materials); Glass fiber reinforced plastics.; Rotary wings.
Notes: Shipping list no.: 98-0818-M.

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