This worksheet is intended to be a quick way to calculate the deflection of a specific cross section of a beam via its elastic equation. Throughout the worksheet E represents the material's Modulus of Elasticity and I represents the Moment of Inertia. A note of caution is that it is the user's responsibility to insure that the corrects units are being used in order to obtain accurate results.
Cantilever beam of length (L) with a concentrated force (P) located at its free end.
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Cantilever beam of length (L) with a uniformly distributed load directed downward along its entire length of magnitude w.
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Cantilever Beam of length (L) with a moment (M) located at its free end. The moment is in a direction that results in the free end of the beam moving down.
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Simply-supported beam of length (L) with a concentrated force (P) at its midpoint. Due to the symmetry of the situation, a cross section at equal distances from the midpoint will have equal deflections. Therefore, the calculations used in this code are only valid for Points_of_Interest less than or equal to one-half the entire length.
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Simply-supported beam of length (L) with a uniformly distributed load along its entire length of magnitude w.
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Simply-supported beam with a length (L) and a moment (M) located above the roller on the right end of the beam. A positive value for this moment is in the counterclockwise direction about the roller.
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Cantilever beam of length (L) with a roller support located beneath its free end. The free end with roller is located at the right end of the plot. The beam is loaded with a uniformly distributed load throughout its entire length of magnitude w.
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