Full Aircraft Dynamic Response by Simplified Structural Models
Author:
Affiliation:
1. Technical University of Turin
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1701
Reference32 articles.
1. 1Euler, L., De curvis elasticis, Lausanne and Geneva: Bousquet, 1744.
2. LXVI. On the correction for shear of the differential equation for transverse vibrations of prismatic bars
3. Non-uniform warping including the effects of torsion and shear forces. Part II: Analytical and numerical applications
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