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I am confused about the cantilever beam |
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| Jan11-13, 01:22 PM | #1 |
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I am confused about the cantilever beam
Hi
For a cantilever beam with a load at its end, flexural rigidity is: EI = m*g*L3 / 3Y Where m=mass, g=gravity, L=length of beam and Y=deflection the natural frequency is f = 1/(2∏) * √ ( 3EI/mL3) Plugging in EI to the formula for f reveals that f depends only on the deflection, Y. If I wanted to predict the frequency, would I therefore only need to measure Y? I am stuck in a circular logic loop because Y depends on m, L and EI but m and L cancel out in f = |
| Jan11-13, 02:42 PM | #2 |
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The deflection depends upon the end load m. The frequency is the √(ratio of elastic forces to inertial ones) ω = √(k/m) and k, the spring constant = Load/Deflection. The equation of motion is (for vubrations in the y direction) [tex]m\frac{{{d^2}y}}{{d{t^2}}} + ky = 0[/tex] |
| Jan11-13, 03:23 PM | #3 |
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I have measurements of m, L, Y and f
there is no relationship between Y and m, Y and L , F and m, F and L there is correlation between Y and f Could the lack of correlation in Y vs m and Y vs L indicate that in my system, EI is the most important predictor of Y and by extension f ? I guess the real problem is that I do not have enough degrees of freedom to determine the effect of EI. |
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