Torque and Angular acceleration

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Homework Help Overview

The discussion revolves around calculating torque in the context of a physics coursework project investigating the torque effect on single propeller planes. The original poster is attempting to understand how to relate angular frequency and angular acceleration to determine the torque produced by a propeller.

Discussion Character

  • Exploratory, Assumption checking

Approaches and Questions Raised

  • The original poster describes their experimental setup and the variables they have, including rpm, length, and mass of the propeller. They express confusion about linking angular frequency with angular acceleration and how to calculate torque from their measurements.
  • Some participants question the original poster's understanding of torque and its relation to the forces acting on the plane, suggesting a need for clarification on the definitions and concepts involved.
  • Others propose that the original poster may need to consider the mechanics of the propeller's connection to the plane and the implications of having a single propeller.

Discussion Status

The discussion is ongoing, with participants providing insights and raising questions about the original poster's understanding of torque and the physical setup. There is no explicit consensus, but some guidance has been offered regarding the need for a clearer understanding of the concepts involved.

Contextual Notes

Participants note potential misunderstandings regarding the definitions of torque and the mechanics of the propeller's operation. The original poster's experimental setup may also be limited by the apparatus used to measure torque.

egroeg93
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Hi all, first time posting so let's see how it goes!

My problems are with a piece of physics coursework I'm doing for my A-level courses. I chose to investigate the 'torque effect' on single propeller planes. (If you are unsure of what this is, its basically Newtons third law, reasoning that when a plane makes a propeller spin, the propeller makes the plane spin).

So i need a way to calculate torque so i can compare it to forces produced on the plane. The setup i used for the experiment is show in the picture:

[PLAIN]http://img827.imageshack.us/img827/1451/physicsforum1.png

Basically, its a suspended mock up of a plane, with a propeller on the front. I'm using a tachometer to measure rpm and scales to measure the 'weight' induced on the wing, which i could convert into a moment.

How can i find the torque of the propeller from this? I've spent ages trawling the internet. The variables i know are: rpm, length and mass of propeller. I also changed the distance alone the 'wings' of the mockup which i measured the force from, using the scales to measure the 'force' the torque effect applied on them.

So what i understand, is:

ω = 2*(pi)*f

a_tangential = Angular acceleration*R

τ = I*α

But how do i link angular frequency with angular acceleration. How could i do this? Could i just use the ideas in the picture and trigonometry?
[URL]http://upload.wikimedia.org/wikipedia/commons/5/56/Acceleration.JPG[/URL]

Many thanks to all!
 
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welcome to pf!

hi egroeg93! welcome to pf! :smile:
egroeg93 said:
… How can i find the torque of the propeller from this? I've spent ages trawling the internet. The variables i know are: rpm, length and mass of propeller. I also changed the distance alone the 'wings' of the mockup which i measured the force from, using the scales to measure the 'force' the torque effect applied on them. …

i think you're misunderstanding both the word "torque" and the way the propellor is connected to the rest of the plane

"torque" can mean a couple (a pair of equal and opposite forces, not in-line), or it can mean the moment of a force

the torque of a propellor is the first type, but your distance x force calculation is the second type

each propellor exerts both a forward horizontal force on the wing, and a couple (a torque) on the propellor shaft

the moments (torques) of the forward horizontal forces of the two propellors (assuming the plane is symmetrical!) cancel out, so those forces don't turn the plane

the propellor shaft isn't connected to the wing or the body, it's connected to the engine … i don't know where that is or how it works, but i assume that either there's something in the engine that "absorbs the recoil", or that there is a torque, but its turning effect is very small since the moment of inertia of the plane is very large, and that that's catered for by a very slight adjustment to the rudder or to the plane's geometry

anyway, i think you'll need an apparatus that incorporates a torsion balance rather than the usual linear one :smile:
 
i was told i could calculate a torque force by my teacher :P

Its modeled on a single propeller plane, so there is no cancelation of forces.

This is a real scenario, and I'm just trying to experiment with it :)
 
egroeg93 said:
i was told i could calculate a torque force by my teacher :P

Its modeled on a single propeller plane, so there is no cancelation of forces.

This is a real scenario, and I'm just trying to experiment with it :)

If there's a single propeller, it's presumably in line with the centre of mass of the plane, so again there should be no moment (torque) about the centre of mass.

I think either you're misunderstanding your teacher's answer, or (s)he's misunderstanding your question.
 

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