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1 Questions
How to make equivalence from real structures?
2 Vibration mode
2.1 Longitudinal vibration
Area: A, Length: L.
Governing equation:
ρutt=Euxx
Frequency of lowest mode under fixed-fixed, free-free condition:
ω=ρELπ
Frequency of lowest mode under fixed-free condition:
ω=ρE2Lπ
Rao, S. S. (2019). Vibration of continuous systems. John Wiley & Sons.
2.2 Flexural vibration
The governing equation is
∂x2∂2(EI∂x2∂2w)+ρA∂t2∂2w=f(x,t)
where
I=Iy=∬Az2dA
Lowest mode for beam simply supported at both ends
ω=(β1l)2(ρAl4EI)1/2=π2(ρAL4EI)1/2.
2.3 Torsional Vibration of Shafts
The governing equation is
∂x∂(GJ∂x∂θ(x,t))+mt(x,t)=I0∂t2∂2θ(x,t)
where I0=ρJ, J=∫Ar2dA. Uniform and without attached mass mt, we have
G∂x2∂2θ(x,t)=ρ∂t2∂2θ(x,t)
Frequency of lowest mode under fixed-fixed, free-free condition:
ω=ρGLπ
Frequency of lowest mode under fixed-free condition:
ω=ρG2Lπ
where
2.4 Shear vibration
Lowest frequency for shear mode is
ω=2bπρμ
where b is half of the thickness d. Or
ω=4dπρμ
where d is the thickness.
2.5 Bending vibration of the plate
Governing equation is
D∇4w+ρhw¨−f=0
in which D represents the flexural rigidity of the plate:
D=12(1−ν2)Eh3
Solution for a simply supported rectangular plate is
ωmn=λmn2(ρhD)1/2=π2[(am)2+(bn)2](ρhD)1/2
The lowest mode (if a>b) is
ω=π2(a1)2(ρhD)1/2
Solution for circular plate is
ωmn=λmn2(ρhD)1/2
where λmn is the solution of the following equation
Im(λa)Jm−1(λa)−Jm(λa)Im−1(λa)=0,m=0,1,2,…
The lowest root is λ01a=3.196. Therefore, the frequency of lowest mode is
ω=(a3.196)2(ρhD)1/2