fundamentals of engineering supplied-reference handbook - Ventech!
fundamentals of engineering supplied-reference handbook - Ventech!
fundamentals of engineering supplied-reference handbook - Ventech!
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UNIAXIAL STRESS-STRAIN<br />
Stress-Strain Curve for Mild Steel<br />
♦<br />
The slope <strong>of</strong> the linear portion <strong>of</strong> the curve equals the<br />
modulus <strong>of</strong> elasticity.<br />
DEFINITIONS<br />
Engineering Strain<br />
ε = ∆L / L0, where<br />
ε = <strong>engineering</strong> strain (units per unit),<br />
∆L = change in length (units) <strong>of</strong> member,<br />
L0 = original length (units) <strong>of</strong> member.<br />
Percent Elongation<br />
⎛ ∆L<br />
⎞<br />
% Elongation = ⎜ × 100<br />
⎝ L ⎟<br />
⎠<br />
o<br />
Percent Reduction in Area (RA)<br />
The % reduction in area from initial area, Ai, to final area,<br />
Af, is:<br />
⎛ Ai − Af<br />
⎞<br />
%RA = ⎜ × 100<br />
⎝ A<br />
⎟<br />
⎠<br />
True Stress is load divided by actual cross-sectional area.<br />
Shear Stress-Strain<br />
γ = τ/G, where<br />
γ = shear strain,<br />
τ = shear stress, and<br />
i<br />
G = shear modulus (constant in linear force-deformation<br />
relationship).<br />
E<br />
G = , where<br />
2 1<br />
( + ν)<br />
E = modulus <strong>of</strong> elasticity<br />
v = Poisson's ratio, and<br />
= – (lateral strain)/(longitudinal strain).<br />
MECHANICS OF MATERIALS<br />
38<br />
Uniaxial Loading and Deformation<br />
σ = P/A, where<br />
σ = stress on the cross section,<br />
P = loading, and<br />
A = cross-sectional area.<br />
ε = δ/L, where<br />
δ = elastic longitudinal deformation and<br />
L = length <strong>of</strong> member.<br />
E<br />
δ =<br />
= σ ε =<br />
PL<br />
AE<br />
P<br />
δ<br />
A<br />
L<br />
THERMAL DEFORMATIONS<br />
δt = αL (Τ – Τo), where<br />
δt = deformation caused by a change in temperature,<br />
α = temperature coefficient <strong>of</strong> expansion,<br />
L = length <strong>of</strong> member,<br />
Τ = final temperature, and<br />
Τo = initial temperature.<br />
CYLINDRICAL PRESSURE VESSEL<br />
Cylindrical Pressure Vessel<br />
For internal pressure only, the stresses at the inside wall are:<br />
2<br />
o<br />
2<br />
o<br />
2<br />
i<br />
2<br />
i<br />
r + r<br />
σt = Pi and 0 > σr<br />
> −Pi<br />
r − r<br />
For external pressure only, the stresses at the outside wall<br />
are:<br />
2<br />
o<br />
2<br />
o<br />
2<br />
i<br />
2<br />
i<br />
r + r<br />
σt = −Po<br />
and 0 > σr<br />
> −Po<br />
, where<br />
r − r<br />
σt = tangential (hoop) stress,<br />
σr = radial stress,<br />
Pi = internal pressure,<br />
Po = external pressure,<br />
ri = inside radius, and<br />
ro = outside radius.<br />
For vessels with end caps, the axial stress is:<br />
σ<br />
a<br />
= Pi<br />
r<br />
2<br />
ri<br />
2 2<br />
o − ri<br />
These are principal stresses.<br />
♦ Flinn, Richard A. & Paul K. Trojan, Engineering Materials & Their Applications,<br />
4th ed., Houghton Mifflin Co., 1990.