NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Tension/torsion loading of composite laminates with free-edge boundary conditionsA finite element analysis of a family of quasi-isotropic graphite/epoxy laminates was conducted for tension, torsion, and combined tension/torsion loading. The model was employed to investigate the effects of delaminations on torsional stiffness and also to evaluate the total strain energy release rates associated with these delaminations.
Document ID
19930043960
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hooper, Steven J. (NASA Langley Research Center Hampton, VA, United States)
Hagemeier, Rick (NASA Langley Research Center Hampton, VA, United States)
Ramaprasad, Srinivasan (Wichita State Univ. KS, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: AHS National Technical Specialists' Meeting on Rotorcraft Structures, Williamsburg, VA, Oct. 29-31, 1991, Proceedings (A93-27951 10-05)
Publisher: American Helicopter Society
Subject Category
Structural Mechanics
Accession Number
93A27957
Funding Number(s)
CONTRACT_GRANT: NAG1-1128
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available