Thrust Formula:
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Definition: This calculator estimates the thrust generated by a propeller or similar device based on fluid dynamics principles.
Purpose: It helps engineers, physicists, and aviation professionals determine the thrust force produced in various fluid environments.
The calculator uses the formula:
Where:
Explanation: The thrust is proportional to fluid density, propeller area, velocity squared, and the thrust coefficient.
Details: Accurate thrust calculation is essential for aircraft design, marine propulsion systems, and any application involving fluid movement.
Tips: Enter the fluid density, propeller area, velocity, and thrust coefficient (default 1.0). All values must be > 0.
Q1: What is a typical thrust coefficient value?
A: For most propellers, CT ranges between 0.5 and 1.5 depending on design and operating conditions.
Q2: What fluid density should I use for air?
A: At sea level, air density is approximately 1.225 kg/m³, but this decreases with altitude.
Q3: How do I calculate propeller area?
A: For circular propellers, use \( A = \pi \times r^2 \) where r is the propeller radius.
Q4: Does this formula work for water propellers?
A: Yes, but remember water density is about 1000 kg/m³, much higher than air.
Q5: Why is velocity squared in the equation?
A: Thrust depends on the kinetic energy of the fluid, which is proportional to velocity squared.