Calculating motor/calculator thrust

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To calculate the thrust generated by a brushless motor and propeller combination for a quadcopter, one can use empirical formulas that consider the propeller's diameter, pitch, and the motor's RPM. A common approach involves using the thrust coefficient, which can be derived from experimental data specific to the propeller type. Additionally, thrust can be estimated using the equation: Thrust = (RPM^2 * Diameter^4 * Pitch) / Constant, where the constant is based on the propeller's characteristics. Users are encouraged to consult specific thrust charts or online calculators for more accurate results tailored to their motor-propeller setup. Accurate thrust calculations are essential for optimizing quadcopter performance.
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Hi I am building a quadro-copter, and I'm curious to know how i can calculate the thrust generated by a motor/propeller combo. The motors are brushless electric motors for which i know the max RPM. The propellers are two bladed for which the diameter and pitch are known. Is there a simple equation for which i can use in order to calculate the thrust/lift a particular combo will produce. Thanks.
 
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I am looking for an answer of the same problem, have you found anything meaningful?
 
Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/
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