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Technology
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Topic:
Euler's Physics (Essay Sample)
Instructions:
The task was about applying the Euler's formula to solve the questions given
source..Content:
Question 1 Assignment 1
Question 1a
Pin-ended Strut
15798806350P00P
Using Euler’s Formula to calculate load likely to cause buckling, PCr=EIπ2L (Freund, 1990)
PCr=200×109 Iπ22=9.872I×1011
I=AL212
I=π×0.03242212=0.00023565M4
PCr=232.64MN
For a load with eccentricity,e=0.007m the maximum load inducing a compressive stress of 200mpa can be calculated as follows;
742950101600WMPeP00WMPeP
Balancing the moments on the free-body diagram it gives (Hill, 1950)
M=P(W+e)
The governing equation for the strut’s transverse displacement w can be illustrated as;
d2ydx2+PEIW=PeEI
M was eliminated using Euler-Bernoulli Theory.
The above equation contains a non-homogeneous term -Fe/EI and its general solution is (Lubliner, 1990),
Wx=Asinkx+Bcoskx-e
Wherek2=PEI. This is denoted as †in the formula sheet. This analysis will use k instead.
The coefficients A and B depend on the boundary conditions. For a simply supported column the boundary conditions are,
W0=wL=o
The solution for the column's displacement is therefore,
W=etankL2sinkx+coskx-1
From this the secant formula is derived to give the maximum value of the displacement as in the equation below
Wmax=eseckl2-1
The maximum stress is therefore given by;
σmax =PA1+ecr2secPLEA2r
Note c is denoted as y in the formula sheet and is the distance from centroidal axis to the extreme fiber on the concave side of the column.
For this question we are given;
σmax =20mpa
E=200GPa
A=Ï€d24
L=2m
d=30mm
e=7mm
We are required to determine P in this equation
r=IA, r is the radius of gyration
From which;
c=7+15=22mm=0.022m
A=π×0.0324=0.00070695m2
r=0.00023565M40.00070695m2 =0.5773503m
20×106=P0.000706951+0.007×0.0220.5773503×0.5773503secP×2200×109 ×0.00070695×2×0.5773503
20×106=P0.000706951+0.000462sec1.22502P×108
11068.06216
20×106=P0.000706951+0.000462sec11068.06216×P
20×106=P0.000706951+0.000462cos11068.06216×P
20×106=P0.000706951-0.00047463cosP
20×106=P0.00070695-0.67138PcosP
14139=P-0.000474634PcosP
14139cosP=PcosP-0.000474634P
PcosP-14139cosP-0.000474634P=0
Using a simple spread sheet program, the value of P can be estimated. The following are some instances of the program results:
Iteration for the first three approximations
P
P
cosP
Pcos(P)
14139cosP
0.000474634P
Sum
100
10
-0.839071
-83.90715291
-11863.63235
0.0474634
11779.67773
110
10.48808848
-0.485981
-53.45796029
-6871.291823
0.05220974
6817.781653
120
10.95445115
-0.041112
-4.933385736
-581.2761743
0.05695608
576.2858325
Further approximations
400
20
0.408082062
163.2328247
5769.872272
0.1898536
-5606.829301
410
20.24845673
0.171050237
70.13059705
2418.479297
0.19459994
-2348.5433
420
20.49390153
-0.07348299
Question 1a
Pin-ended Strut
15798806350P00P
Using Euler’s Formula to calculate load likely to cause buckling, PCr=EIπ2L (Freund, 1990)
PCr=200×109 Iπ22=9.872I×1011
I=AL212
I=π×0.03242212=0.00023565M4
PCr=232.64MN
For a load with eccentricity,e=0.007m the maximum load inducing a compressive stress of 200mpa can be calculated as follows;
742950101600WMPeP00WMPeP
Balancing the moments on the free-body diagram it gives (Hill, 1950)
M=P(W+e)
The governing equation for the strut’s transverse displacement w can be illustrated as;
d2ydx2+PEIW=PeEI
M was eliminated using Euler-Bernoulli Theory.
The above equation contains a non-homogeneous term -Fe/EI and its general solution is (Lubliner, 1990),
Wx=Asinkx+Bcoskx-e
Wherek2=PEI. This is denoted as †in the formula sheet. This analysis will use k instead.
The coefficients A and B depend on the boundary conditions. For a simply supported column the boundary conditions are,
W0=wL=o
The solution for the column's displacement is therefore,
W=etankL2sinkx+coskx-1
From this the secant formula is derived to give the maximum value of the displacement as in the equation below
Wmax=eseckl2-1
The maximum stress is therefore given by;
σmax =PA1+ecr2secPLEA2r
Note c is denoted as y in the formula sheet and is the distance from centroidal axis to the extreme fiber on the concave side of the column.
For this question we are given;
σmax =20mpa
E=200GPa
A=Ï€d24
L=2m
d=30mm
e=7mm
We are required to determine P in this equation
r=IA, r is the radius of gyration
From which;
c=7+15=22mm=0.022m
A=π×0.0324=0.00070695m2
r=0.00023565M40.00070695m2 =0.5773503m
20×106=P0.000706951+0.007×0.0220.5773503×0.5773503secP×2200×109 ×0.00070695×2×0.5773503
20×106=P0.000706951+0.000462sec1.22502P×108
11068.06216
20×106=P0.000706951+0.000462sec11068.06216×P
20×106=P0.000706951+0.000462cos11068.06216×P
20×106=P0.000706951-0.00047463cosP
20×106=P0.00070695-0.67138PcosP
14139=P-0.000474634PcosP
14139cosP=PcosP-0.000474634P
PcosP-14139cosP-0.000474634P=0
Using a simple spread sheet program, the value of P can be estimated. The following are some instances of the program results:
Iteration for the first three approximations
P
P
cosP
Pcos(P)
14139cosP
0.000474634P
Sum
100
10
-0.839071
-83.90715291
-11863.63235
0.0474634
11779.67773
110
10.48808848
-0.485981
-53.45796029
-6871.291823
0.05220974
6817.781653
120
10.95445115
-0.041112
-4.933385736
-581.2761743
0.05695608
576.2858325
Further approximations
400
20
0.408082062
163.2328247
5769.872272
0.1898536
-5606.829301
410
20.24845673
0.171050237
70.13059705
2418.479297
0.19459994
-2348.5433
420
20.49390153
-0.07348299
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