higher order mode wave propagation in duct yan li机械系统与振动国家重点实验室...
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Higher order mode wave propagation in duct
Yan Li
机械系统与振动国家重点实验室 机械系统与振动国家重点实验室 上海交通大学,上海交通大学, 200240200240 ,上海,上海
Research background
Higher order mode • In a rectangular duct
• In a circular duct
• In expansion chamber
Conclustion
OutlineOutline
Research BackgroundResearch Background
Sound transmission characteristics of duct system
• Building, automotive and aeronautic noise control
• Bends, constrictions, expansions & side branches
• Many study at low frequency
• Inaccurate estimates at first cut-on frequency
• Higher order mode wave propagation
Research background
Higher order mode wave propagation • In a rectangular duct
• In a circular duct
• In expansion chamber
OutlineOutline
Higher order mode in a rectangular Higher order mode in a rectangular ductduct
)cos()cos(~ ykxkAp nm
0)cos()sin(~ ykakBv nmx
Boundary condition at the wall of the duct requires:
0)sin()cos(~ bkxkCv nmy
Transmission wave number for (m, n) mode:
0])/()/([ 2/12220,, bnamkk nmz
,2,1,0, mmakm
,2,1,0, nnbkn
2/122 ])/()/)[(2/( bnamcfc
Cutoff frequencies:
a x
b z
Higher order mode in a rectangular Higher order mode in a rectangular ductduct
Fig. 1. Nodal lines for transverse pressure distribution in a rectangular duct up to m=3, n=3 higher order mode
the number of pressure nodal lines in the x direction
the number of pressure nodal lines in the y direction
Higher order mode in a circular ductHigher order mode in a circular duct
)(~ krAJp
0)(~ ' kRBJv m
Fig. 2. Bessel function of the first kind for order m=0,1,2. Boundary condition met when slopes goes to zero at wall of
circular duct
Rx
y
z
Fig. 3. Nodal lines for transverse pressure distribution in circular duct up to m=3, n=3 higher node with preferred
notation for m, n
Higher order mode in a circular ductHigher order mode in a circular duct
kR
Higher order mode in a circular ductHigher order mode in a circular duct
Cutoff frequency• First asymmetric mode m=1,n=0
• First circularly symmetric/radial mode m=0, n=1
DcDcfc /586.0/84.1
DcDcfc /22.1/83.3
Effects in expansion chamberEffects in expansion chamber
Fig. 4. Schematic of illustrations of instantaneous axial pressure distribution for higher mode propagation,
tunneling and leakage of one mode
Effects in expansion chamberEffects in expansion chamber
Fig. 5. Insertion loss measurements on expansion chamber using broad band noise excitation on impedance tube with anechoic
termination (c=345m/s)
Research background
Higher order mode • In a rectangular duct
• In a circular duct
• In expansion chamber
Conclustion
OutlineOutline
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