Calculating Propeller Thrust Using Given Data

AI Thread Summary
To calculate thrust produced by a propeller in flight, the required propeller induced velocity is often missing, complicating the process. Key known variables include propeller efficiency, indicated and true airspeed, altitude temperature and pressure, engine torque, propeller diameter, and rotational speed. The discussion emphasizes that thrust distribution calculations involve iterative methods. A participant offers assistance based on their experience with propeller performance design during a project. For further guidance, they suggest using specific relationships found on an external resource.
mohd_omr
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i need to calculate thrust produced by a propeller whilst flying, using the data show below. all equations i have come across require the propeller induced velocity which is not given.

things i know;
-propeller efficiency
-indicated and true airspeed of aircraft
-temp. and pressure at flying altitude
-engine torque
-propeller diameter
-propeller rotating speed

i have tried serching the forum but couldn't find a relevant equation.
 
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propeller efficiency and thrust are functions of airspeed.
 
Dear buddy,

It takes some iteration to calculate thrust distribution for propeller. However, I can help u to do that coz during my final year project, I've assigned to design and find performance of the propeller itself.

U can give anything that u know abt the propeller, and I will try to help u on that. Email me at solehan85@gmail.com
 
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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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