Flight Dynamics Analysis of Periodically Forced Rotorcraft Model
Author:
Affiliation:
1. University of Bristol
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6634
Reference23 articles.
1. Bifurcation Analysis of Nonlinear Aircraft Dynamics
2. Analysis and control of bifurcation phenomena in aircraft flight
3. Application of bifurcation theory to the high-angle-of-attack dynamics of the F-14
4. Application of bifurcation methods to nonlinear flight dynamics problems
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. On the nonlinear dynamics of a rotor in autorotation: a combined experimental and numerical approach;Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences;2015-09-28
2. A Combined Numerical/Experimental Continuation Approach Applied to Nonlinear Rotor Dynamics;Progress in Industrial Mathematics at ECMI 2008;2010
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