Cantilever Boundary Condition, Deflections, and Stresses of Sandwich Beams
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139-4307
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1738
Reference12 articles.
1. LXVI. On the correction for shear of the differential equation for transverse vibrations of prismatic bars
2. X. On the transverse vibrations of bars of uniform cross-section
3. The Effect of Rotatory Inertia and of Shear Deformation on the Frequency and Normal Mode Equations of Uniform Beams With Simple End Conditions
4. Allen, H. G., Analysis and Design of Structural Sandwich Panels, Pergamon, Oxford, 1969, pp.21-33.
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