BEAM SUPPORTED WITH UNIFORM LOAD

BEAM SUPPORTED WITH UNIFORM LOAD
Static calculations
* * *

OBJECT:

n° decimal =

INSERT DATA
for decimals put the point
q = overload + own weight daN/ml
L = cm
J = moment of inertia cm⁴
W = resistance modulus cm³
E = elasticity module daN/cm²
f permissible = L / cm
permissible Tension = daN/cm²
x = (0.00 < x < L) = cm

RESULTS

Ra = Rb = q L/2 = daN
Ma = Mb = 0 = daNm
Mab = q L²/8 = daNm
Mx = q x (L - x ) /2= daNm
Tx = q (L - 2 x) /2 = daN
Ta = - Tb = q L/2 = daN
Tb = daN
A-B = tension found in the middle = Ma-b/W = daN/cm²
f = arrow found in the middle = 5 q L⁴/384 E J = cm
arrow at point x of your choice = cm
permissible arrow = cm

rotations

alpha in x = rotation in x of your choice (0 ÷ L) degrees
alpha in A = rotation in A or B degrees

1 daN = 1 Kg