Date post: | 09-Jul-2016 |
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Inputs Beam Dimensions
b (in)
h (in)
round_tube 24.0 3.5001.000
User Input Variables are Red Bold
Select Beam Cross Section from Menu
Total Beam Length (in)
Buckling Load Calculations
One_Fixed_One_Free 2.00
Cantilever Beam Calculations
case_2 200.0
*Note: The length L used is the "total beam length" from cell D14
Material Properties Via: https://www.botfeeder.ca/abs-vs-pla/
http://www.matweb.com/
Select Beam End Conditions (using the same beam from the above
section)
Resulting K value
Select Beam Loading Conditions (using the same beam from the above
section)
Point Load F (lbs)
case 1
case 2
case 3
case 4
case 5
case 6
1 2
Cross-Section of Beam
0.292
3.865
3.500
Weight (lb) 23.86126,000210,00084,00076,44121,000
Solid Rectangle(or square)Moment of Inertia
about Ixc (in^4)Polar Moment of Area (in^3)Cross-Section Area (in^2)
Yield Tensile Strength (lb)Ultimate Tensile Strength (lb)Shear Strength (lb) (single shear):Torsional Strength (in-lb) Bending Moment (in-lb)
K= 0.69
Buckling Load (lb) 304,413
Cantilever Beam Equations
Cantilever Beam Inputs: 1,000.0 0.0
#REF!
Buckling Load End Conditions (load applied to long axis)
Force: F(lbs)
Distributed Force: P(psi)
Solid Rectangle(or square)
Deflection: y (in)Angle
(deg)Maximum Moment (in-lb)
#REF!
Properties data sources: http://www.azom.com/http://www.speedymetals.com/http://www.matweb.com/
a 875.0000b 3,500.0000c 7,000.0000de 8,573.2141f 34,292.8564g 51,439.2846
Maximum Force (lbs)
Inputs Beam Dimensions Beam Material Properties
t (in)
0.216 A36 60,000
Beam Mechanical Properties
### Moment of Inertia about Ixc (in^4)
### Polar Moment of Area: J (in^3)
### Cross-Section Area: A (in^2)
### Weight: W (lb)
### Yield Tensile Strength (lb)
### Ultimate Tensile Strength (lb)
### Transverse Shear Strength (single shear) (lb)
### Torsional Strength (in-lb)
### Bending Moment (in-lb)
User Input Variables are Red Bold
Select Beam Material from
Menu
Ultimate Tensile Strength
(psi)
Buckling Load Calculations
3,149,016
Cantilever Beam Calculations
200.00.0000 0.0001
*Note: The length L used is the "total beam length" from cell D14
https://www.botfeeder.ca/abs-vs-pla/
Buckling Load (lbs)
Distributed Load P (psi)
Deflection: y (in)
Angle (deg)
3 4 5 6
Cross-Section of Beam
Solid Circle0.245 7.366
2.451 14.732
1.757 9.621
11.98 65.5863,266 346,361
105,443 577,26831,633 259,77048,477 303,06617,627 151,533
Hollow Rectangle(or square)
255,515 7,688,102
Cantilever Beam Equations
0.0 ### A
Solid Circle
#REF! #REF!
K = 2.0 One end fixed, one end freeK = 1.0 Both ends pinned K = 0.69 One end fixed, one end pinnedK = 0.50 Both ends fixed
Distributed Force: P(psi)
Length: L
(ref from above)
(inches)
Beam Condition (A, B, C, D, E, F, G)
Hollow Rectangle(or square)
#REF! #REF!
734.4469 6,313.86492,937.7877 25,255.45975,875.5753 50,510.9194
7,196.0808 61,862.989528,784.3231 247,451.957943,176.4847 371,177.9368
Beam Material Properties
36,000 36,000 0.284 29,000,000
Beam Mechanical Properties
Moment of Inertia about Ixc (in^4) 3.0172
Polar Moment of Area: J (in^3) 6.0343
Cross-Section Area: A (in^2) 2.2285
Weight: W (lb) 15.19
Yield Tensile Strength (lb) 80,225
Ultimate Tensile Strength (lb) 133,708
Transverse Shear Strength (single shear) (lb) 40,112
Torsional Strength (in-lb) 124,134
Bending Moment (in-lb) 62,067
User Input Variables are Red Bold
Yield Strength (psi)
Shear Strength (psi)
Density (lb/in^3)
Youngs Modulus
(psi)
Buckling Load Calculations
Cantilever Beam Calculations
1,200
*Note: The length L used is the "total beam length" from cell D14
Maximum Moment (in-lb)
7 8 9 10
Cross-Section of Beam
Hollow Circle angle3.017 0.0462
6.034 1.192
2.228 0.925
15.19 6.3180,225 33,312
133,708 55,52140,112 Sorry, not available!
124,134 23,57062,067 2,078
3,149,016 48,221
Cantilever Beam Equations
Hollow Circle
#REF!
#REF!
2,586.134210,344.536920,689.0738
25,338.8370101,355.3481152,033.0222
Beam Material Properties
11,500,000
Modulus of Rigidity
(psi)
11
Cross-Section of Beam
0.285 1
1.829 2
2.5673
17.50 492,424 5
154,041 64,417 7
36,180 820,549 9
I beam(normal
orientation)
297,871
Cantilever Beam Equations
#REF!
H beam(normal
orientation)
#REF!
856.19393,424.77576,849.5514
8,388.952933,555.811850,333.7177
1 rectangle_bar
3 rectangle_tube
5 round_bar
7 round_tube
11 i_beam
9 angle
rectangle_bar 0.000 0 convert thickness to b1 & b2
rectangle_tube b1 (in) h1 (in)
0.000 3.068 0.568
1.000 b2 (in) h2 (in)
1.642 0.284
Solid Triangle
0.097
0.146
1.750
11.93
63,000
105,000
N/A
7,875
5,247
101,471
Solid Triangle
#REF!
z 2.05y 0.8
cy 0.2cx 1.45iyc 1.145
4
6061
2011
4140
A36
304
1144
TGP 1045
*1018 cold rolled
1018
*110
Copper
Cast Iron
Bronze
UHMW PE
PVC
ABS
PLA
Polycarbinate
1
match #
Density lb/in³ Youngs modulus
45,000 40,000 27,000 0.098 10,000,000
55,000 44,000 33,000 0.098 10,000,000
70,000 60,000 42,000 0.284 29,000,000
60,000 36,000 36,000 0.284 29,000,000
73,200 31,200 43,920 0.284 29,000,000
115,000 100,000 69,000 0.284 29,000,000
92,000 48,000 55,200 0.284 29,000,000
63,800 53,700 38,280 0.284 29,000,000
32,000 10,000 19,200 0.324 16,000,000
40,000 32,000 24,000 0.284 14,500,000
35,000 20,000 21,000 0.304 14,500,000
3,000 1,500 1,800 0.034 NA
6,000 3,000 3,600 0.050 490,000
Tensile Strength
(PSI)
Yield Strength
(PSI)
Shear Strength
(PSI)
9,000 4,500 5,400 0.046 NA
6,500 6,200 3,900 0.043 320,000
8,383 7,300 5,030 0.045 478,624
12
3
4
2 match
y
0 1 case_1 0.0004392 case_2 2.742934219E-0053 case_3 6.857335547E-006
0 4 case_4 0.00016457610 5 case_5 1.714333887E-0050 6 case_6 0.0019749126
F
Modulus of Rigidity
3,800,000
3,800,000
11,500,000
11,500,000
10,900,000
10,900,000
10,900,000
10,900,000
6,500,000
5,900,000
6,500,000
NA
NA otfeeder.ca/abs-vs-pla/
NA
152,290
350,000
1 matched
One_Fixed_One_Free 2.00Both_Pinned 1.00
One_Fixed_One_Pinned 0.69
Both_Fixed 0.50
teta Mmax
0.0006583042 48000.000082288 1200
None 6000.0002194347 57600
5.485868437945E-005 14400None 9600