Solve for maximum deflection of a cantilever or simply supported beam under a point or distributed load, using the matching formula with every substitution shown.
You are a structural engineering tutor who knows the single most common mistake in this topic isn't the arithmetic, it's grabbing the wrong formula because the support condition and the load pattern weren't checked first. A cantilever with a point load and a simply supported beam with the same point load deflect by wildly different amounts, and no amount of careful multiplication fixes starting from the wrong equation. Work in [MODE:select:solve for maximum deflection,explain the four standard cases with a worked example] mode. Set the support condition to [SUPPORT:select:cantilever fixed at one end,simply supported at both ends] and the load type to [LOAD_TYPE:select:point load,uniformly distributed load]. Give me the beam's values in [BEAM_VALUES?], covering the load, the span length, the modulus of elasticity, and the moment of inertia of the cross-section. If I left this blank, ask me for the specific values instead of assuming a beam. Before any arithmetic, state which of the four standard formulas applies given [SUPPORT] and [LOAD_TYPE], and write it out in full with each symbol named: a cantilever with a point load at the free end deflects as load times length cubed, divided by 3 times E times I. A cantilever with a uniform load deflects as load times length cubed, divided by 8 times E times I. A simply supported beam with a central point load deflects as load times length cubed, divided by 48 times E times I. A simply supported beam with a uniform load deflects as load times length cubed, divided by 384 times E times I. Confirm this formula is the one you're using before substituting a single number. Substitute the values from [BEAM_VALUES] into that formula on their own line, keeping every unit visible, then compute the result. If the moment of inertia wasn't given directly but the cross-section shape was, such as a rectangular or circular section, work it out first as its own separate step before substituting it into the deflection formula, since folding two calculations into one is where a units mismatch usually hides. If I chose explain the four standard cases with a worked example, lay out all four formulas side by side first, and point out the two comparisons that matter most: a cantilever deflects roughly ten times more than a simply supported beam under the same load and span, and a uniformly distributed load produces less deflection than the same total load concentrated at a single point. Then pick one case, using [BEAM_VALUES] if they give usable numbers or a simple example if I left that blank, and solve it with the same explicit substitution method above. Whatever mode you ran, close by sanity-checking the result against the beam's own span. If the calculated deflection is larger than the span itself, or negative, something in the formula selection or the substitution went wrong, so say that plainly and trace back to find it instead of reporting an implausible number as final.
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Get Early AccessFour different formulas cover a cantilever versus a simply supported beam under a point load versus a uniform load, and grabbing the wrong one is where most beam deflection homework actually goes wrong, not the arithmetic that follows.
This tool checks your [SUPPORT] and [LOAD_TYPE] first and states which of the four standard formulas applies before touching a single number. A cantilever with a point load uses load times length cubed over 3 E I. A simply supported beam with a uniform load uses load times length cubed over 384 E I, and so on for the other two cases. Give it your [BEAM_VALUES] and, if the moment of inertia wasn't given directly, it gets calculated first as its own step from the cross-section shape, since folding that into the final substitution is exactly where a units mismatch hides.
Solve directly for the maximum deflection, or see all four standard cases laid out side by side with a worked example, including the two comparisons that actually matter: a cantilever deflects roughly ten times more than a simply supported beam under the same load and span, and a uniform load deflects less than the same total load concentrated at one point.
Run it in the Dock Editor to keep the worked solution with your problem set, or paste it into ChatGPT, Claude, or Gemini. Once you need the actual stress at a point in that same beam, the shear stress and bending stress solver picks up from the deflected shape.
Copy this into ChatGPT, Claude, Gemini, or the Dock Editor, then set [MODE] to solving for maximum deflection or seeing all four standard cases explained.
Choose [SUPPORT] as cantilever or simply supported, and [LOAD_TYPE] as a point load or a uniformly distributed load, since these two choices determine which formula applies.
Fill in [BEAM_VALUES] with the load, span length, modulus of elasticity, and moment of inertia. If the moment of inertia isn't known yet, describe the cross-section shape instead.
The output states which of the four standard deflection formulas applies to your support and load combination before substituting a single value.
The output confirms the deflection is smaller than the beam's own span. A result larger than the span or negative signals a formula or substitution mistake worth tracing back.
Get a fully worked deflection calculation for homework with the correct formula identified up front, instead of guessing between four similar-looking equations.
Compare how support conditions and load types change deflection side by side, useful for building intuition before an exam.
Generate a worked example with all four standard cases laid out together as a model answer or handout.
Estimate how much a shelf or beam will sag under a known load before committing to a material and span.
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