Drone Speed Equation:
From: | To: |
The drone speed equation calculates the theoretical maximum speed of a drone based on its thrust, the air density, and the propeller area. This equation is fundamental in drone design and performance analysis.
The calculator uses the drone speed equation:
Where:
Explanation: The equation shows that speed increases with higher thrust and decreases with higher air density or larger propeller area.
Details: Understanding drone speed is crucial for flight planning, battery life estimation, and ensuring safe operation within performance limits.
Tips: Enter thrust in Newtons, air density in kg/m³ (1.225 kg/m³ at sea level), and total propeller area in m². All values must be positive numbers.
Q1: What is typical drone thrust?
A: Small consumer drones typically produce 5-20N of thrust, while larger commercial drones can produce 50-200N.
Q2: How does air density affect drone speed?
A: Higher density (colder air or lower altitude) reduces maximum speed, while lower density (hot air or high altitude) increases it.
Q3: What's the practical maximum speed for drones?
A: Most consumer drones max out around 15-25 m/s (54-90 km/h) due to aerodynamic limitations and safety concerns.
Q4: Does this equation account for drag?
A: No, this is the theoretical maximum. Actual speed will be lower due to aerodynamic drag and other factors.
Q5: How to calculate total propeller area?
A: For n propellers of diameter d: Area = n × π × (d/2)²