Columns + Kinematics and Stresses

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1
Slenderness Ratio
$SR=\frac{L_e}{k}$
effective length / radius of gyration
2
Radius of Gyration
$k=\sqrt{\frac{I}{A}}
3
Effective Length
$L_e=KL
4
Normal Stress
$S=\frac{F}{A}
5
Factor of Safety
$FS=\frac{S_{ultimate}}{S_{design}}
6
Normal Stress w/ D and d
$S=\frac{F}{\frac{π}{4}(D^2-d^2)}
7
Thickness
$t=\frac{D-d}{2}$
$t=r_o-r_i
8
Shear Stress
$S=\frac{F}{πDt}
9
Bolt Stress
$S_{bolt}=\frac{\frac{PA_{cylinder}}{N_{bolts}}}{A_{bolt}}
10
Proportional Limit
11
Modulus of Elasticity of Steel
$E_{steel}=30x10^6 psi
12
Modulus of Elasticity of Aluminum$
$E_{Al}=\frac{1}{3}E_{steel}
13
Modulus of Rigidity of Steel
$G=12x10^6psi
14
Poissons Ratio and 2big
$v=-\frac{Ɛ_{lateral}}{Ɛ_{longitudinal}}$

$E=2(v+1)G
15
Axial Deformation
$δ=\frac{FL}{AE}
16
Elongation
$Ɛ=\frac{δ}{L}
17
Deformation Due to Own Weight
$δ=\frac{ρgL^2}{2E}
18
Dilatation
$e=Ɛ_x+Ɛ_y+Ɛ_z$

$e=\frac{F}{AE}(1-2v)
19
Thermal Elongation and Thermal Stress
$δ=αL∆T$

$S=Eα∆T$

$\alpha=6.51x10^{-6}°
20
Bending/Flexural Stress
$S_b=\frac{Mc}{I_x}
21
Flexural/Bending Stress Square Cantilever Beam
$S_b=\frac{6M}{bh²}
22
Flexural/Bending Stress Circular Cantilever
$S_b=\frac{32M}{πD³}
23
$S_b=\frac{3V}{2bh}
24
Maximum Moment 2 formulas
$M_{max}=\frac{ωL^2}{8}$

$M_{max}=\frac{PL}{4}
25
Band Saw
$S=\frac{Et}{D}
26
Slenderness Ratio
$SR=\frac{L_e}{k}
27
Effective Length and End Coefficient
$L_e=KL$
$C=\frac{1}{K^2}
28
Max Moment
$M_{max}=\frac{PL}{4}$

$M_{max}=\frac{\omega L^2}{8}
29
Moment of Inertia Square

$I_x=\frac{bh^3}{12}
30
Moment of Inertia Triangle
$I_x=\frac{bh^3}{36}
31
Moment of Inertia Circle
$I_x=\frac{\pi r^4}{4}$
$I_x=\frac{\pi D^4}{64}
32
Radius of Gyration
$k=\sqrt{\frac{I}{A}}
33
Buckling Formula: Euler's
$F_c=\frac{π^2EI}{L_e^2}
34
Buckling Formula: JB Johnson
$F_c=S_yA\left[1-\frac{S_y(L_e/k)^2}{4π^2E}\right]
35
Maximum Shear Stress (Combined Stresses)
$Ss_{max}=\sqrt{\left(\frac{S_x-S_y}{2}\right)^2+S_s^2}
36
Maximum Stress (Combined)
$S_{max}=\frac{S_x+S_y}{2}+Ss_{max}
37
Minimum Stress (Combined)
$S_{min}=\frac{S_x+S_y}{2}-Ss_{max}
38
Degree of Freedom
$DOF=3(N-1)-2L_{pair}-H_{pair}$

$DOF=3(N-1)-2L_{pair}
39
Alternating Stress
$S_a=\frac{S_x-S_y}{2}
40
Mean Stress
$S_m=\frac{S_x+S_y}{2}
41
For Static Failure, FS 2 formulas
$FS=\frac{S_y}{S_m}$

$FS=\frac{S_u}{S_m}
42
Instantaneous Center
$v=r\omega$

$\omega=\frac{v_A}{r_A}=\frac{v_B}{r_B}
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