A direct analytical beam formulation is developed for predicting the effective elastic stiffnesses and corresponding load deformation behavior of tailored composite box‐beams. Deformation of the beam is described by extension, bending, torsion, transverse shearing, and torsion‐related
warping. Evaluation and validation of the analysis are conducted by correlation with both exprimental results and detailed finite element solutions. The analysis is evaluated for thin‐walled composite beams with no elastic coupling, designs with varying degrees of extension‐torsion
and bending‐shear couplings, and designs with bending‐torsion and extension‐shear coupling. The analysis is performed well over a wide range of test cases, generally predicting beam deformations within 10 percent of detailed finite element solutions. The importance of
three non‐classical structural phenomena is systematically investigated for coupled composite beams. Torsion‐related warping can substantially influence torsion and coupled torsion deformations: twist of a symmetric layup box‐beam under a tip bending load can increase
up to 200 percent due to warping. Couplings associated with transverse shear deformations can significantly alter the elastic response of tailored composite box‐beams: effective bending stiffness of highly coupled anti‐symmetric layup beams can be reduced more than 30 percent.
Two‐dimensional elasticity of the plies is also very important to the accuracy of composite box‐beam analysis; load deflection results for anti‐symmetric layup beams can be altered by 30–100 percent by not accounting for this elastic behavior.
No Reference information available - sign in for access.
No Citation information available - sign in for access.
No Supplementary Data.
No Article Media
No Metrics
Document Type: Research Article
Affiliations:
Center for Rotorcraft Education and Research, Dept. of Aerospace Engineering, University of Maryland, College Park, Md.
Publication date:
01 July 1991
More about this publication?
The Journal of the AHS is the world's only scientific journal dedicated to vertical flight technology. It is a peer-reviewed technical journal published quarterly by The Vertical Flight Society and presents innovative papers covering the state-of-the-art in all disciplines of VTOL design, research and development. (Please note that VFS members receive significant discounts on articles and subscriptions.)
Journal subscribers who are VFS members log in here if you are not already logged in.
Authors can find submission guidelines and related information on the VFS website.