Drone Lift Equation:
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The drone lift equation estimates the total lifting capacity of a multirotor drone based on propeller characteristics and operating conditions. It accounts for the number of propellers, their diameter, rotation speed, air density, and thrust coefficient.
The calculator uses the drone lift equation:
Where:
Explanation: The equation shows that lift increases with the fourth power of propeller diameter and square of RPM, making these the most critical factors for lift capacity.
Details: Accurate lift estimation is crucial for drone design, payload capacity determination, and ensuring safe operation within performance limits.
Tips: Enter all required parameters. Default values are provided for air density (1.225 kg/m³) and thrust coefficient (0.1). For precise results, measure your propeller's actual Ct value.
Q1: Why does propeller diameter have such a large effect?
A: Lift is proportional to diameter^4 because larger propellers move more air and do so more efficiently.
Q2: What's a typical thrust coefficient value?
A: Most drone propellers have Ct between 0.05-0.2. Higher values indicate more efficient thrust generation.
Q3: How does air density affect lift?
A: Lift is directly proportional to air density. Drones produce less lift at higher altitudes where air is thinner.
Q4: What's the relationship between lift and thrust?
A: For hovering drones, total lift must equal total weight (including payload). Additional thrust is needed for climbing.
Q5: How can I increase my drone's lift capacity?
A: Increase propeller diameter (most effective), add more propellers, increase RPM, or use more efficient propellers (higher Ct).