Encyclopaedia Britannica, 11th Edition, Volume 4, Part 3 / "Brescia" to "Bulgaria"

by Various

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component of the resultant (tangent to the curve) will be unaltered; the vertical component V will be simply the sum of the loads between O and F, or wx. In the triangle FDC, let FD be tangent to the curve, FC vertical, and DC horizontal; these three sides will necessarily be proportional respectively to the resultant tension along the chain at F, the vertical force V passing through the point D, and the horizontal tension at O; hence

H : V = DC : FC = wx²/2y : wx = x/2 : y,

hence DC is the half of OC, proving the curve to be a parabola.

The value of R, the tension at any point at a distance x from the vertex, is obtained from the equation

R² = H²+V² = w²x4/4y²+w²x²,

or,

2 . . . R = wx?(1+x²/4y²).

Let i be the angle between the tangent at any point having the co-ordinates x and y measured from the vertex, then

3 . . . tan i = 2y/x.

Let the length of half the parabolic chain be called s, then

4 . . . s = x+2y²/3x.

The following is the approximate expression for the relation between a change ?s in the length of the half chain and the corresponding change ?y in the dip:?

s+?s = x+(2/3x) {y²+2y?y+(?y)²} = x+2y²/3x+4y?y/3x+2?y²/3x,

or, neglecting the last term,

5 . . . ?s = 4y?y/3x,

and

6 . . . ?y = 3x?s/4y.

From these equations the deflection produced by any given stress on the chains or by a change of temperature can be calculated.

Fig. 71.--Beam bent by external loads. Fig. 71.

36. Deflection of Girders.? Let fig. 71 represent a beam bent by external loads. Let the origin O be taken at the lowest point of the bent beam. Then the deviation y = DE of the neutral axis of the bent beam at any point D from the axis OX is given by the relation

d²y
/
dx²
= M
/
EI

where M is the bending moment and I the amount of inertia of the beam at D, and E is the coefficient of elasticity. It is usually accurate enough in deflection calculations to take for I the moment of inertia at the centre of the beam and to consider it constant for the length of the beam. Then

dy
/
dx
= 1
/
EI
?Mdx
y = 1
/
EI
??Mdx².

The integration can be performed when M is expressed in terms of x. Thus for a beam supported at the ends and loaded with w per inch length M = w(a²-x²), where a is the half span. Then the deflection at the centre is the value of y for x = a, and is

? = 5
/
24
wa4
/
EI
.

The radius of curvature of the beam at D is given by the relation

R = EI/M.

Fig. 72.--Graphic Method of finding Deflection
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