Calculator Usage Guide
- Enter the velocity of the object relative to the fluid (m/s)
- Enter the drag coefficient (Cd) of the object. This value depends on the shape of the object and the flow conditions. For a smooth sphere at low Reynolds numbers, it's approximately 0.47.
- Enter the reference area (A), which is typically the cross-sectional area perpendicular to the direction of motion.
- Click the "Calculate" button to compute the drag force, resultant pressure, and pressure coefficient.
- Click "Reset" to clear all input fields and start over.
Understanding the Drag Equation
The drag force (FD) is calculated using the following formula:
FD = 0.5 × ρ × v² × Cd × A
Where:
- FD = Drag Force (Newtons, N)
- ρ = Fluid density (kg/m³) - Default value is for air at sea level (1.225 kg/m³)
- v = Velocity (meters per second, m/s)
- Cd = Drag Coefficient (dimensionless)
- A = Reference Area (square meters, m²)
Practical Applications
This calculator is useful in various fields including:
- Aerospace engineering for aircraft and spacecraft design
- Automotive engineering for vehicle aerodynamics
- Fluid dynamics for analyzing flow around objects
- Sports science for analyzing the aerodynamics of sports equipment