where
RA = reaction force in A (N, lb)
F = single acting force in B (N, lb)
at the fixed end can be expressed as
Mmax = MA
= - F L (1b)
where
MA = maximum moment in A (Nm, Nmm, lb in)
L = length of beam (m, mm, in)
at the end of the cantilever beam can be expressed as
δB = F L3 / (3 E I) (1c)
where
δB = maximum deflection in B (m, mm, in)
E = modulus of elasticity (N/m2 (Pa), N/mm2, lb/in2 (psi))
I = moment of Inertia (m4, mm4, in4)
b = length between B and C (m, mm, in)
The stress in a bending beam can be expressed as
σ = y M / I (1d)
where
σ = stress (Pa (N/m2), N/mm2, psi)
y = distance to point from neutral axis (m, mm, in)
M = bending moment (Nm, lb in)
I = moment of Inertia (m4, mm4, in4)
The maximum moment in a cantilever beam is at the fixed point and the maximum stress can be calculated by combining 1b and 1d to
σmax = ymax F L / I (1e)
The maximum moment at the fixed end of a UB 305 x 127 x 42 beam steel flange cantilever beam 5000 mm long, with moment of inertia 8196 cm4(81960000 mm4), modulus of elasticity 200 GPa (200000 N/mm2) and with a single load 3000 N at the end can be calculated as
Mmax = (3000 N) (5000 mm)
= 1.5 107 Nmm
= 1.5 104 Nm
The maximum deflection at the free end can be calculated as
δB = (3000 N) (5000 mm)3 / (3 (2 105 N/mm2) (8.196 107 mm4))
= 7.6 mm
The height of the beam is 300 mm and the distance of the extreme point to the neutral axis is 150 mm. The maximum stress in the beam can be calculated as
σmax = (150 mm) (3000 N) (5000 mm) / (8.196 107 mm4)
= 27.4 (N/mm2)
= 27.4 106 (N/m2, Pa)
= 27.4 MPa
Maximum stress is way below the ultimate tensile strength for most steel.
at the fixed end can be expressed as:
RA = F (2a)
where
RA = reaction force in A (N, lb)
F = single acting force in B (N, lb)
at the fixed end can be expressed as
Mmax = MA
= - F a (2b)
where
MA = maximum moment in A (N.m, N.mm, lb.in)
a = length between A and B (m, mm, in)
at the end of the cantilever beam can be expressed as
δC = (F a3 / (3 E I)) (1 + 3 b / 2 a) (2c)
where
δC = maximum deflection in C (m, mm, in)
E = modulus of elasticity (N/m2 (Pa), N/mm2, lb/in2 (psi))
I = moment of Inertia (m4, mm4, in4)
b = length between B and C (m, mm, in)
at the action of the single force can be expressed as
δB = F a3 / (3 E I) (2d)
where
δB = maximum deflection in B (m, mm, in)
The maximum stress can be calculated by combining 1d and 2b to
σmax = ymax F a / I (2e)
A generic calculator - be consistent and use metric values based on m or mm, or imperial values based on inches. Default typical values are in metric mm.
at the fixed end can be expressed as:
RA = q L (3a)
where
RA = reaction force in A (N, lb)
q = uniform distributed load (N/m, N/mm, lb/in)
L = length of cantilever beam (m, mm, in)
at the fixed end can be expressed as
MA = - q L2 / 2 (3b)
at the end can be expressed as
δB = q L4 / (8 E I) (3c)
where
δB = maximum deflection in B (m, mm, in)
A generic calculator - use metric values based on m or mm, or imperial values based on inches. Default typical values are in metric mm.
If more than one point load and/or uniform load are acting on a cantilever beam - the resulting maximum moment at the fixed end A and the resulting maximum deflection at end B can be calculated by summarizing the maximum moment in A and maximum deflection in B for each point and/or uniform load.
at the fixed end can be expressed as:
RA = q L / 2 (4a)
where
RA = reaction force in A (N, lb)
q = declining distributed load - max value at A - zero at B (N/m, lb/ft)
at the fixed end can be expressed as
Mmax = MA
= - q L2 / 6 (4b)
where
MA = maximum moment in A (N.m, N.mm, lb.in)
L = length of beam (m, mm, in)
at the end of the cantilever beam can be expressed as
δB = q L4 / (30 E I) (4c)
where
δB = maximum deflection in B (m, mm, in)
E = modulus of elasticity (N/m2 (Pa), N/mm2, lb/in2 (psi))
I = moment of Inertia (m4, mm4, in4)
Deflection and stress, moment of inertia, section modulus and technical information of beams and columns.
Typical cross sections and their Area Moment of Inertia.
Calculate beam load and supporting forces.
Stress, deflections and supporting loads.
Supporting loads, moments and deflections.
Supporting loads, stress and deflections.
Calculate position of center mass.
Moments and reaction support forces with distributed or point loads.
Calculate the acting forces and moments when elevating drawbridges or beams.
Properties of HE-B profiled steel beams.
Use levers to magnify forces.
The Mass Moment of Inertia vs. mass of object, it's shape and relative point of rotation - the Radius of Gyration.
Weight, cross sectional area, moments of inertia - Imperial units
Dimensions and static parameters of steel angles with equal legs - metric units.
Dimensions and static parameters of steel angles with unequal legs - imperial units.
Dimensions and static parameters of steel angles with unequal legs - metric units.
Stiffness is resistance to deflection.
Support reactions and bending moments.
Common types of trusses.
Stress and deformation of vertical beams due to own weight.
Weight supported by a double or triple wood headers.
Young's Modulus (or Tensile Modulus alt. Modulus of Elasticity) and Ultimate Tensile Strength and Yield Strength for materials like steel, glass, wood and many more.
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