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Fixed-pinned beam - Two equal concentrated loads symmetrically placed Calculator















Formula

Property Formula
Deflection (\(y_{AC}\)) \(y_{AC} = \frac{Px^2}{12EI L^2} [(3a^2 - 3aL - 2L^2)(L-x) + 2L(3a^2 - 3aL + L^2)]\)
Deflection (\(y_{CD}\)) \(y_{CD} = \frac{-Pa(3(L-a)(L-x)^3 - 6L^2(L-x)^2)}{12EI L^2 a^2} + \frac{-Pa[3L^2(L+a)(L-x) - 2L^2 a]}{12EI L^2}\)
Deflection (\(y_{DB}\)) \(y_{DB} = \frac{-P(L-x)}{12EI L^2} [(3aL - 3a^2 - 2L^2)(L-x)^2 + 3aL^2(L-a)]\)
Slope (\(\theta_{AC}\)) \(\theta_{AC} = \frac{Px}{12EI L^2} [(3a^2 - 3aL - 2L^2)(2L - 3x) + 4L(3a^2 - 3aL + L^2)]\)
Slope (\(\theta_{CD}\)) \(\theta_{CD} = \frac{-Pa}{4EI L^2} [-3(L-a)(L-x)^2 + 4L^2(L-x) - L^2(L+a)]\)
Slope (\(\theta_{DB}\)) \(\theta_{DB} = \frac{P}{4EI L^2} [(3aL - 3a^2 - 2L^2)(L-x)^2 + aL^2(L-a)]\)
Moment (\(M_{AC}\)) \(M_{AC} = \frac{P}{2L^2} [3a^2 L - 3aL^2 + x(2L^2 + 3aL - 3a^2)]\)
Moment (\(M_{CD}\)) \(M_{CD} = \frac{-Pa}{2L^2} [3(L-a)(L-x) - 2L^2]\)
Moment (\(M_{DB}\)) \(M_{DB} = \frac{-P(L-x)}{2L^2} [3aL - 3a^2 - 2L^2]\)
Shear (\(V_{AC}\)) \(V_{AC} = \frac{P}{2L^2} (2L^2 + 3aL - 3a^2)\)
Shear (\(V_{CD}\)) \(V_{CD} = \frac{3Pa(L-a)}{2L^2}\)
Shear (\(V_{DB}\)) \(V_{DB} = \frac{P}{2L^2} (3aL - 3a^2 - 2L^2)\)
Reaction (\(R_A\)) \(R_A = \frac{P}{2L^2} (2L^2 + 3aL - 3a^2)\)
Reaction (\(R_B\)) \(R_B = \frac{P}{2L^2} (3a^2 + 2L^2 - 3aL)\)

Definitions

Symbol Physical quantity Units
E·I Flexural rigidity N·m², Pa·m⁴
y Deflection or deformation m
θ Slope, Angle of rotation -
x Distance from support (origin) m
L Length of beam (without overhang) m
M Moment, Bending moment, Couple moment applied N·m
P Concentrated load, Point load, Concentrated force N
w Distributed load, Load per unit length N/m
R Reaction load, reaction force N
V Shear force, shear N
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