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General Design Principles for DuPont Engineering Polymers - Module

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Form of bar;<br />

manner of loading and support<br />

Uni<strong>for</strong>m straight bar under end load<br />

One end free, other end fixed<br />

Uni<strong>for</strong>m straight bar under end load<br />

Both ends hinged<br />

l<br />

l<br />

P<br />

P<br />

P<br />

Table 4.04. Buckling of Columns, Rings and Arches<br />

E = modulus of elasticity, I = moment of inertia of cross section about central axis perpendicular to plane of buckling.<br />

All dimensions are in inches, all <strong>for</strong>ces in pounds, all angles in radians.<br />

Uni<strong>for</strong>m straight bar under end load<br />

One end fixed, other end hinged and<br />

horizontally constrained over fixed end<br />

0.7 l<br />

0.3 l<br />

Uni<strong>for</strong>m circular ring under uni<strong>for</strong>m radial<br />

pressure p lb/in. Mean radius of ring r.<br />

Uni<strong>for</strong>m circular arch under uni<strong>for</strong>m radial<br />

pressure p lb/in. Mean radius r.<br />

Ends hinged<br />

Uni<strong>for</strong>m circular arch under uni<strong>for</strong>m radial<br />

pressure p lb/in. Mean radius r.<br />

Ends fixed<br />

r<br />

P<br />

2�<br />

P<br />

2�<br />

P<br />

P' = π 2 El<br />

4 l 2<br />

P' = π 2 El<br />

l 2<br />

Formulas <strong>for</strong> critical load P', critical unit load p', critical torque T', critical bending moment M',<br />

or critical combination of loads at which elastic buckling occurs<br />

P' = π 2 El<br />

(0.7 l ) 2<br />

p' =<br />

p' =<br />

3 El<br />

r 2<br />

( – 1 )<br />

2 El π<br />

r 3 �2 (For symmetrical arch of any <strong>for</strong>m under central concentrated loading see Ref. 40)<br />

p' = El (k 2 – 1)<br />

r 3<br />

Where k depends on α and is found by trial from the equation: k tan α cot kα = 1 or from the following<br />

table:<br />

α = 15° 30° 45° 60° 75° 90° 120° 180°<br />

k = 17.2 8.62 5.80 4.37 3.50 3.00 2.36 2.00<br />

21

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