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Applications of Beams and Bending
(Credit for many illustrations is given to McGraw Hill publishers and an array ofinternet search results)
Parallel Reading
Section 6.4 Design of Beams for StrengthSection 6.5 Flexural Stress in nonhomogeneous beams(Do Reading Assignment Problem Set 6B)
Chapter 6
Lets Try Using Our Radius of Curvature Formula
Old McDonald had a beam
The beam had a Young’s ModulusOf 165 GPa
If was acted on by a 3 KN*mBending couple
What are the maximum tensile and compressive stresses and radius of curvature?
Our Key Formulas
Obviously we are going nowhere with thisUntil we get the Inertia of our beam
Getting I
We previously got our centroid using a weighted average of area but nowwe are after the second moment - I
Getting the inertia of each of the componentrectangles about their own axis would notbe a trick. There is a formula for that.
20 mm90 mm
40 mm
30 mm Of course we want the moment about theCentroid axis
Fortunately We Have the Parallel Axis Theorem
000,6012
*90 203
200,259*1800 122
The moment of inertia of an element aboutA different axis is the moment of inertia ofThe element around its own axis
90
20
+
180012
Plus the area of the element time theDistance between the axis squared.
000,6012
*90 203
So Work Through and Get the Inertia
1800
90
2012
From component #1
1200
30
4018
From component #2
1800
1200
Stresses Go Down Easy Now
Our basic formula
Compression side on bottom σ max = -131.3 MPa (Negative is for compression)
Tension side on top σ max = 76 MPa (Positive is for tension)
Now for the Radius of Curvature
Lets Try Bending a Beam
How much of a bending moment can I puton this puppy before the stress goes outof tolerance?
Our basic formula
1.8
(Interesting note Wood is usually weaker incompression than tension)
Getting a Hold of I
86412
*6 123
Our Solution Formula
We know the critical stress is going to be tension(Compression is the high strength measure foralmost all materials)
We know the neutral plain passesThrough the centroid
6 in So the distance y from the centroid toThe point of maximum compression mustbe 6 inches
Set Up Our Equation
lbsinMy
I*000,288
6
864*2000*
Lets Do a Bit of Reinforcing
We’ll put a reinforcing plate on the bottom ofthe beam and see how much it can take now.
1.8
For Composite Materials Life Get Tougher
It is no longer true that theNeutral axis or plane passesthrough the centroid.
Finding the Neutral Axis
Start by getting the ratio of the Young’s Modulus of theTwo materials(Steel will be much more resistant to strain than wood)
Now Weight Each Component Area According to Young’s Modulus
Remember steel hasa Young’s Modulus of16 times that of wood.
Now Use That Weighted Area to Apply a Weight to the Centroid of
Each Component Area
6 in
0.25 in
Now Divide Through By Weighted Area to Find the Neutral Plane
3.758 in
CompressionArea
TensionSide
Avoid Confusion
What we just found was the neutral axis –The axis of the first moment.
This is NOT the second moment or momentof inertia. Do not confuse the calculations!
Now We Will Take the Inertia Moment of Each Component
Around the Neutral Axis
Wood area (I1) aroundNeutral Axis
Steel Area (I2 ) aroundNeutral Axis
Obviously I’m using theParallel Axis Theorem
Now We Will Use Our Young’s Modulus Weighted Stress Formula
Lets see what kind of stress our wood compressionArea will take.
8.242 in
lbsinMyn
I*2.688,454
242.8*1
77.1873*2000
*
*
So Lets See What the Tension Side Will Take
9.600911258.4*111.16
77.1873*000,22M
4.258
Comparison
• Will Our New Beam be limited by compression or tension– Wood Compression limit 454,688 in*lbs– Tension Limit for Steel 600,912 in*lbs– Obviously the wood at the top will crush out first –
limit is 454,688 in*lbs
• But without the plate the limit was 288,000 in*lbs
A little steel goes a long ways
Now Lets Try a Few FE Style Problems
We know we get this answer by taking the area weighted average of theCentroids of each component area.
6 cm2
10 cm2
5.5 cm
Of course picking off centroidsand areas of rectangles iseasy prey.
2.5 cm
Take That Area Weighted Average
3.625 cm Pick C
Take That Area Weighted Average
3.625 cm Pick C
Lets Do One With a Composite Beam
We will weight the two componentAreas by their Young Modulus.Then we will weight the centroidsof the two component areas bytheir weighted areas.
Lets Get the Weighted Area
Area = 4 cm2
2 cm
2 cm
0.125 cm
Steel Area Equivalent = 2*0.125*20 = 5 cm2
Identify the Centroids of the Component Areas With Respect to
the Beam Bottom
0.125
2 cm
1.125 cm
0.0625 cm
Now weight them by the weighted areas
1.125* 4 + 0.0625* 5 = 4.8125
Now divide through by the totalArea
4.8125/(4 + 5) = 0.535 cm
Pick B
Assignment 15
Do problems 6.5-8 and 6.5-14(note that these are the same problem, but you are being ask to solve it byTwo different methods).
For each step in your work show the formulas and explain the logic andApproach you are using to work toward a solution. Circle your answer atThe end. Warning – explaining your work is a key part of the answer.Failure to include step by step explanations and your work will get youMarked wrong – even if the answer is correct.