20.01.2015 Views

Example Stress Analysis 2

Example Stress Analysis 2

Example Stress Analysis 2

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

MET 210W<br />

<strong>Stress</strong> <strong>Analysis</strong> 2 <strong>Example</strong>s Page 1 of 4<br />

1. The shaft shown rotates at 240 rpm. Determine the<br />

power input to the system at the middle gear. If the shaft<br />

is solid with a diameter of 1.2 inches, determine the<br />

torsional shear stress at C and at D.<br />

Internal Torque<br />

Reaction, T (lb·in)<br />

-1500” # 600” #<br />

Power Calculations:<br />

HP<br />

T n<br />

= 63025<br />

=<br />

Polar Moment of Inertia:<br />

4<br />

4<br />

π D π (1.2" )<br />

J = = =<br />

32 32<br />

in<br />

4<br />

Shear <strong>Stress</strong> at C:<br />

Shear <strong>Stress</strong> at D:<br />

If the distance between gear E and the middle gear is 12 inches, find the angle of twist between the two<br />

gears. The shaft is steel and G = 11.5 x 10 6 psi.


MET 210W<br />

<strong>Stress</strong> <strong>Analysis</strong> 2 <strong>Example</strong>s Page 2 of 4<br />

2. The triangular shaft has a 1500 inch-pound torque applied<br />

as shown. Determine the maximum shear stress in the<br />

shaft and the angle of twist of the free end with respect to<br />

the fixed end.<br />

Section Properties:<br />

a = 1.5”<br />

From Mott, Figure 3-10, Page 99:<br />

Q = .050a 3 and K = .0217a 4


MET 210W<br />

<strong>Stress</strong> <strong>Analysis</strong> 2 <strong>Example</strong>s Page 3 of 4<br />

3. The elliptical aluminum tube is subjected to the torque<br />

shown. Dimension b is 1 inch and the wall thickness<br />

is .10 inches. Find the angle of twist in a 48 inch<br />

length of the tube.


MET 210W<br />

<strong>Stress</strong> <strong>Analysis</strong> 2 <strong>Example</strong>s Page 4 of 4<br />

4. Determine the stresses acting at points A and B shown. Show the<br />

stresses on stress elements.<br />

Section Properties from Statics:<br />

X<br />

I x = 7486226 mm 4<br />

y = 99.08 mm<br />

Reactions at Cut:<br />

M CUT<br />

800 mm<br />

F CUT<br />

V CUT<br />

3.6 kN<br />

FBD at Cut<br />

4.8 kN

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!