Fig. 8: Samaras are robust to mass addition.
From: Maple samara flight is robust to morphological perturbation and united by a classic drag model
a Reduced velocity Vd/Vd0 vs reduced mass m/m0, b reduced angular velocity ω/ω0 vs reduced mass m/m0, c reduced cone angle θ/θ0 vs reduced mass ratio m/m0 vs, and d drag force to samara weight mg.
