Equation of motion: $ma = mg - \frac{1}{2}\rho C_d A v^2$
Terminal velocity: $v_t = \sqrt{\dfrac{2mg}{\rho C_d A}}$
Reynolds number: $Re = \dfrac{\rho v D}{\mu}$
Adjust mass, drag coefficient, and cross-section area to visualize falling motion in real time. Explore presets from skydiver to raindrop and see how terminal velocity changes.
Equation of motion: $ma = mg - \frac{1}{2}\rho C_d A v^2$
Terminal velocity: $v_t = \sqrt{\dfrac{2mg}{\rho C_d A}}$
Reynolds number: $Re = \dfrac{\rho v D}{\mu}$
The core physics is Newton's second law applied to a falling object. The net force is weight ($mg$) minus the air drag force, which is proportional to the square of the velocity for high-speed motion. This gives us the equation of motion.
$$ma = mg - \frac{1}{2}\rho C_d A v^2$$Where $m$ is mass (kg), $a$ is acceleration (m/s²), $g$ is gravity (9.81 m/s²), $\rho$ is air density (kg/m³), $C_d$ is the drag coefficient, $A$ is the cross-sectional area (m²), and $v$ is velocity (m/s).
Terminal velocity ($v_t$) occurs when acceleration is zero. Setting $a=0$ in the equation above and solving for $v$ gives us the terminal velocity formula. This is the key result you can test directly in the simulator.
$$v_t = \sqrt{\dfrac{2mg}{\rho C_d A}}$$This shows mathematically what we discussed: $v_t$ increases with mass ($m$) and decreases with air density ($\rho$), drag coefficient ($C_d$), and area ($A$).
Skydiving & Parachute Design: Skydivers control their terminal velocity by changing their cross-sectional area and drag coefficient. By arching their body, they can reach speeds over 50 m/s. Opening the parachute massively increases $A$ and $C_d$, reducing $v_t$ to a safe ~5 m/s for landing.
Vehicle Aerodynamics: Automotive engineers use wind tunnels and CAE software to minimize a car's drag coefficient ($C_d$) to improve fuel efficiency at high speeds. A lower $C_d$ means the engine works less to overcome air resistance.
Meteorology & Raindrop Physics: A raindrop's terminal velocity (typically 5-9 m/s) determines how fast precipitation reaches the ground. This depends on the drop's size (affecting $m$ and $A$) and shape, which is modeled with a specific $C_d$.
Particle Settling in Industry: In chemical engineering, the terminal velocity concept is used to design separators and settling chambers. For example, calculating how fast dust or powder particles fall through air or liquid is crucial for air pollution control and product processing.
There are a few key points you should be especially mindful of to master this simulator. First, the drag coefficient Cd is not a constant determined solely by shape. For example, while we mentioned a baseball's Cd is about 0.3, this is for a certain velocity range. In reality, it varies with speed, ball spin, and surface roughness. The simulator simplifies this to a constant value, so please treat it strictly as a tool for "grasping trends."
Next, how to interpret the cross-sectional area A. The cross-sectional area here refers to the projected area as seen from the direction of motion. For instance, the air resistance experienced by a skydiver in a spread-eagle position (free-fall) versus a head-first diving position (track position) is completely different. This is because the cross-sectional area A changes dramatically. If you try changing only the area while keeping mass constant in the simulator, you should clearly see its impact on terminal velocity.
Finally, understand the fundamental limitation that reality is far more complex than one-dimensional fall. This calculation uses an idealized model of "falling straight down." For actual baseball breaking balls or lateral movement (drift) in skydiving, forces not handled by this tool—like lift and lateral drag—play a significant role. Please use this as a first step to learn the "basic behavior of air resistance."
A skydiver with mass 80 kg, belly-to-earth area 0.55 m², and Cd 1.15 in standard air (ρ = 1.225 kg/m³): terminal velocity vt = √(2×80×9.81/(1.225×0.55×1.15)) ≈ 53 m/s. Time to 90% vt ≈ 8.2 seconds. At terminal velocity, kinetic energy = 0.5×80×53² ≈ 112 kJ. Reynolds number Re ≈ 1.8×10⁶ (turbulent regime).