Calculate the moment of inertia of a uniform triangular lamina of mass

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Homework Help Overview

The discussion revolves around calculating the moment of inertia of a uniform triangular lamina, specifically an isosceles triangle with a given base and height, about its axis of symmetry. Participants are exploring the mathematical formulation and integration techniques required for this calculation.

Discussion Character

  • Exploratory, Mathematical reasoning, Assumption checking

Approaches and Questions Raised

  • Participants discuss various methods for deriving the moment of inertia, including the use of double integrals. There are attempts to express mass in terms of dimensions of the triangle and to set up integrals based on the geometry of the shape. Some participants question the correctness of initial results and explore alternative formulations.

Discussion Status

The discussion has seen participants sharing their attempts and results, with some expressing uncertainty about the correctness of their findings. There is acknowledgment of different approaches, including coding the problem in software for verification. While some participants have arrived at a result, there is no explicit consensus on the final answer, and further exploration of the topic continues.

Contextual Notes

Some participants note potential errors in their initial calculations and the need to clarify assumptions regarding the distribution of mass and the impact of triangle dimensions on the moment of inertia.

mattgad
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Homework Statement



Calculate the moment of inertia of a uniform triangular lamina of mass m in the shape of an isosceles triangle with base 2b and height h, about its axis of symmetry.

The Attempt at a Solution



I've tried various things for this and never get the correct answer, 1/2*m*b^2.
I'm beginning to think this may involve a double integral.

Thanks.
 
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I don't think ½mb² is the right result.

Here is a similar example I did earlier:
https://www.physicsforums.com/showthread.php?t=278184

In this case I think you would attack the sum of the x²*dm by observing that you can construct m in terms of x as something like h*(1-x/b) so that you arrive at an integral over an expression something like (hx² -x³/b)*dx.

At the end you will be able note that the area of the lamina triangle times the implied density ρ yields you an M total mass in the product that defines your moment.
 
I have coded this problem as a double integral in Maple.

> x(y):=b*(1-y/h);
> rho:=M/(b*h);
> dJ:=int(rho*z^2,z=0..x(y));
> J:=2*int(dJ,y=0..h);

In the first line, the right boundary is defined.
In the second line, the mass density is expressed.
In the third line, the integration in the x-direction is performed from the axis of symmetry to the right edge
In the fourth line, the integration is performed in the y-direction from bottom to top. The result is M*b^2/6. It is reasonable that h should not be in the result. The altitude should not affect this function, only the base width which describes how far the mass is distributed off the axis of rotation.
 
Happily algebraic methods arrive at the same result.
 
I did actually mean to put mb^2 / 6 in my first post. Thanks for replies. Last night I managed to get it myself as well after spotting errors in my work. Thanks.
 
how about the inertia product of this problem?
 

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