Modal analysis of isotropic and composite wings with the Dynamic Transfer Matrix Method
Author:
Affiliation:
1. Military Technical College,Aircraft Mechanics Department,Cairo,Egypt
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9942273/9942362/09942434.pdf?arnumber=9942434
Reference22 articles.
1. Explicit analytical expressions for frequency equation and mode shapes of composite beams
2. Principles of Composite Material Mechanics
3. Coupled bending-torsional dynamic stiffness matrix for beam elements
4. EXPLICIT FREQUENCY EQUATION AND MODE SHAPES OF A CANTILEVER BEAM COUPLED IN BENDING AND TORSION
5. Thin-walled composite beams under bending, torsional, and extensional loads
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