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Civil

Simply supported end rotation under full-span uniform load

Slope at either support of a simply supported prismatic beam under a uniform downward load w over the whole span.

Ref
CIV-21
Rev
v1
Field
Civil
Result
|θend| [rad]

For a simply supported beam under full-span uniform load the end slope is wL³/(24EI). The two ends rotate by the same amount in opposite directions, so the page reports the magnitude. It is the basis for bearing rotations and for slope-deflection calculations, and it is three times the end slope of the same beam under a midspan point load of equal total.

Slope at either support of a simply supported prismatic beam under a uniform downward load w over the whole span. The two end rotations are equal in size and opposite in sign; the page gives the magnitude. Constant EI, small rotations, in radians.

Calculator

Solve for
rad
N/m
100100,000
m
130
N·m²
1,000,0001e9
  • Rotation in degrees0.1719 °
  • Midspan deflection, 5wL⁴/(384EI)0.005625 m
  • Total load, wL60,000 N

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

End rotation (rad) current value 0.003 rad
LSpanKey driver
1.39e-50.375
EIFlexural rigidity
9e-50.09
wLoad intensity
3e-50.03
  • Each support end rotates 0.1719°, and the midspan deflects 5.625 mm.
  • A bearing that must allow this rotation needs a tilt capacity of at least 3 milliradians, plus allowance for construction tolerance.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (rad)Local stepChange in result
L Span1 to 30 m1.389e-50.3750.375+10%+33.1 %
EI Flexural rigidity1,000,000 to 1e9 N·m²9e-50.090.08991+10%−9.09 %
w Load intensity100 to 100,000 N/m3e-50.030.02997+10%+10 %

Sweep of Span

Span (m)End rotation (rad)
11.389e-5
4.6250.001374
8.250.007799
11.880.02326
15.50.05172
19.130.09716
22.750.1635
26.380.2548
300.375

Sweep one variable

End rotation (rad)Hover, touch, or use the arrow keys on the chart
00.10.20.30.4 51015202530 Span (m) now 0.003

Variables and how each one contributes

|θend|

End rotation

Result · rad

What the equation gives you. Everything else feeds it.

w

Load intensity

N/m · typical 100 to 100,000

The uniform load intensity, in N/m. Scales the rotation in direct proportion. Raising it by 10 % (to 11,000) moves the result by +10 %, from 0.003 to 0.0033 rad.

L

Span

m · typical 1 to 30

The span, in m. Raises the rotation with the cube of the span. Raising it by 10 % (to 6.6) moves the result by +33.1 %, from 0.003 to 0.003993 rad.

EI

Flexural rigidity

N·m² · typical 1,000,000 to 1e9

The flexural rigidity, in N·m². A stiffer beam rotates less in inverse proportion. Raising it by 10 % (to 3.3×107) moves the result by −9.09 %, from 0.003 to 0.002727 rad.

Worked example with the values above

  1. L³ = 216 m³ and 24EI = 7.2×108 N·m².
  2. Numerator: wL³ = 10,000 × 216 = 2,160,000.
  3. |θ| = 2,160,000 / 7.2×108 = 0.003 rad.

Assumptions and limits

  • Slender prismatic beam of constant EI with small deflections and rotations.
  • Shear deformation is neglected, which is acceptable for span-to-depth ratios above about 10.

Common mistakes

  • Using EI in the wrong units, such as kN·m² with loads in N.
  • Applying a midspan formula to a deflection at another point.
  • Using a uniform-load coefficient for a triangular or partial load.

Statistics and uncertainty

The deflection formulas are exact for Euler–Bernoulli beams in small deflection, so the dominant uncertainty is EI itself: modulus varies by ±10 %, cracked concrete can halve it, and joint flexibility adds more. Measured deflections often differ from calculated ones by 10 % to 30 %, and long-term creep adds to that.

Where it is used

  • Checking serviceability limits such as span/360 for deflection.
  • Estimating tip movements of cantilevers and bearing rotations.

Maths you need

  • Elastic curve: EI y″ = M(x)
  • Superposition: deflections from separate loads add in a linear structure
  • Flexural rigidity: EI, the product of modulus and second moment of area

Related formulas

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