3D Terminal Velocity Manifold for a NACA-0012Your model is disabled. For more details go to Edit properties3D Model
The terminal velocity manifold in extended phase space for a airfoil with the lift and drag characteristics of a NACA-0012 airfoil from . The blue points along the manifold represent stable equilibrium points and the red points represent saddle equilibria. Blue and red values along the manifold show the magnitude of acceleration.
 Nave Jr., Gary K. and Ross, Shane D. (2018) “Global phase space structures in a model of passive descent.” arXiv preprint arXiv:1804.05099 https://arxiv.org/abs/1804.05099