Date of download: 7/28/2017
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From: Operational Parameter Study of Aircraft Dynamics on the Ground
J. Comput. Nonlinear Dynam. 2010;5(2):021007-021007-11. doi:10.1115/1.4000797
Figure Legend:
The bifurcation curves L and H for a light aircraft and for thrust levels of (a) T=14%, (b) T=15.4%, and (c) T=16% are shown in
projection onto the (δ,Vx)-plane (first column), onto the (δ,CG)-plane (second column), and onto the (Vx,CG)-plane (third column).
Note that the Vx-axis has been reversed in the third column to remain consistent with the surfaces, as plotted in Fig. . The black
dots in panels (b) represent degenerate Bogdanov–Takens points and in panels (c) two non-degenerate Bogdanov–Takens points.
Compare panels (a) and (c) with Fig. , respectively.