Kinematics & Ballistics

Quadratic Aerodynamic Drag & Terminal Velocity Ballistics Lab

Integrate non-analytic aerodynamic drag equations via 4th-order Runge-Kutta and verify KE + PE + E_thermal = Constant.

Real-Time RK4 Kinematic / Dynamical Waveform Recorder

Physical Principles & Mathematical Derivation

F_drag = −kd × |v| × v, KE + PE + E_thermal = E_initial

At realistic speeds, turbulent air drag scales with speed squared, coupling horizontal and vertical equations of motion through |v| = √(vx² + vy²) so closed-form algebraic solutions no longer exist — making RK4 numerical integration essential.

Questions & Concepts

What physical equation governs Quadratic Aerodynamic Drag & Terminal Velocity Ballistics Lab?

F_drag = −kd × |v| × v, KE + PE + E_thermal = E_initial — At realistic speeds, turbulent air drag scales with speed squared, coupling horizontal and vertical equations of motion through |v| = √(vx² + vy²) so closed-form algebraic solutions no longer exist — making RK4 numerical integration essential.

How are the equations of motion integrated in this simulation?

Nonlinear differential equations are integrated at 240–300 Hz substeps using classical 4th-order Runge-Kutta (RK4) to maintain strict Hamiltonian energy accuracy.

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