Uncertainty and Sensitivity Analysis of Bifurcation Loci Characterizing Nonlinear Landing-Gear Dynamics
Author:
Affiliation:
1. University of Bristol, Bristol, England BS8 1TR, United Kingdom
2. Siemens PLM Software, 3001 Leuven, Belgium
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034252
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1. Continuation of Higher-Order Harmonic Balance Solutions for Nonlinear Aeroelastic Systems
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5. Fast Bayesian identification of a class of elastic weakly nonlinear systems using backbone curves
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