Projectile Motion with Quadratic Air Drag
Model aerodynamic deceleration using coupled ODEs
Model the trajectory of a spherical projectile under the influence of gravity and non-linear aerodynamic air resistance.
Governing Equations & Formulation
Parameters: Mass $m = 0.145\text{ kg}$, initial speed $v_0 = 45\text{ m/s}$, launch angle $\theta = 45^\circ$, drag constant $c = 0.0015\text{ kg/m}$, $g = 9.81\text{ m/s}^2$.