Torsion (cont.) - Faculty of Aerospace Engineering
Torsion (cont.) - Faculty of Aerospace Engineering Torsion (cont.) - Faculty of Aerospace Engineering
The Interlaminar Conditions Stress resultants (equilibrium): Displacements (compatibility): Faculty of Aerospace Eng., Technion - I.I.T. 8
The proposed analytical methodology St. Venant’s Semi-Inverse methodology (“solution hypothesis”). The three auxiliary problems of plane deformation (biharmonic BVP). The bending and torsion functions (harmonic BVP). Faculty of Aerospace Eng., Technion - I.I.T. 9
- Page 1 and 2: Non-Homogeneous Composite Beams und
- Page 3 and 4: Motivation • Fiber-reinforced com
- Page 5 and 6: Notation Tip loads Surface loads Bo
- Page 7: Non-Homogeneous Cross-Section Defin
- Page 11 and 12: Transverse Bending Force Effect ben
- Page 13 and 14: The three auxiliary problems of pla
- Page 15 and 16: Source of the Three Auxiliary Plane
- Page 17 and 18: Displacement: Strain: Stress: Field
- Page 19 and 20: Example: Torsion of Non-Homogenous
- Page 21 and 22: Torsion (cont.) Stress component τ
- Page 23 and 24: Bending of Non-Homogenous Beam y x
- Page 25 and 26: Bending of Non-Homogenous Beam (con
- Page 27 and 28: Bending of Non-Homogenous Beam (con
- Page 29 and 30: Solution for Py x σ xx y x Py σ y
- Page 31 and 32: Solution for Py (cont.) x τ yz y x
The Interlaminar Conditions<br />
Stress resultants (equilibrium):<br />
Displacements (compatibility):<br />
<strong>Faculty</strong> <strong>of</strong> <strong>Aerospace</strong> Eng., Technion - I.I.T.<br />
8
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