Built -in (Encastre) beams are fixed at both ends.
Continuous beams, which are beams with more than two supports and covering more
than one span, are not statically determinate using the static equilibrium laws.

e = strain

σ = stress (N/m^{2})

E = Young's Modulus = σ /e (N/m^{2})

y = distance of surface from neutral surface (m).

R = Radius of neutral axis (m).

I = Moment of Inertia (m^{4} - more normally cm^{4})

Z = section modulus = I/y _{max}(m^{3} - more normally cm^{3})

M = Moment (Nm)

w = Distributed load on beam (kg/m) or (N/m as force units)

W = total load on beam (kg ) or (N as force units)

F= Concentrated force on beam (N)

L = length of beam (m)

x = distance along beam (m)

A built in beam is normally considered to be horizontal with both ends built-in at
the same level and with zero slope at both ends. A loaded built in beam
has a moment at both ends and normally the maximum moments at at one or both of the
two end joints.

A built in beam is generally much stronger than a simply supported beam of the same
geometry. The bending moment reduces along the beam
and changes sign at points of contraflexure between the supports and the load.
A typical built-in beam is shown below.

It is not normally possible to determine the bending moments and the resulting stress using static equilibrium.
Deflection calculations are often used to enable the moments to be determined.

Repeating section from Beam Theory

It has been proved ref Shear Bending that dM/dx = S and dS/dx = -w = d^{2}M /dx

Where S = the shear force M is the moment and w is the distributed load /unit length of beam. Therefore

Using the above beam as an example...

Using the above equations the bending moment, shear force, deflection, slope can be determined at
any point along the beam.

M = EI d ^{2}y/dx ^{2} = w(- 6x^{2}+6lx -l^{2})/12

at x = 0 & l then M = -wl^{2} /12 and at x = l/2 then M = wl^{2} /24

S = EI d ^{3}y/dx ^{3} = w(l/2 - x)

at x = 0 then S = w.l/2 at x = l then S = -w.l/2

This type of beam is normally considered using the Clapeyron's Theorem ( Three Moments theorem)

The three moments theorem identifies the relationship between the bending moments found at three consecutive
supports in a continuous beam. This is achieved by evaluating the slope of of the beam
at the end where the two spans join. The slopes are expressed in terms of the three moments
and the supported loads which are then equated and the resulting equations solved.

This relationship for spans with supports at the same height and with spans of constant section
results in the following expression. _{}

If the beams has a different section for each span then the more general expression applies as shown below.

Example Areas and x _{1} value calculations.

Example 1)

This simple example is a two span continuous beam with the ends simple supported, therefore
with no moments at the end support points..

2) Shear Forces

3) Diagrams

Example 2)

This simple example is a three span continuous beam with the ends simple supported, therefore with no moments at the end support points..

The values of A_{1},x_{1},A_{2}, and x_{2} are calculated using the methods above..

- Three Moment equation for continuous beam analysis...Very advanced paper download
- Mitcalc...Excel based software including coded beam calculations
- Chapter 6 Moment Distribution...Chapter of Book including detailed information