Abstract

Musical flue instruments such as the pipe organ and flute mainly consist of the acoustic pipe resonance and the jet impinging against the pipe edge. The edge tone is used to be considered as the energy source coupling to the pipe resonance. However, jet-drive models describing the complex jet/pipe interaction were proposed in the late 1960s. Such models were more developed and then improved to the discrete-vortex model and vortex-layer model by introducing fluid-dynamical viewpoint, particularly vortex sound theory on acoustic energy generation and dissipation. Generally, the discrete-vortex model is well applied to thick jets, while the jet-drive model and the vortex-layer model are valid to thin jets used in most flue instruments. The acoustically induced vortex (acoustic vortex) is observed near the amplitude saturation with the aid of flow visualization and is regarded as the final sound dissipation agent. On the other hand, vortex layers consisting of very small vortices along both sides of the jet are visualized by the phase-locked PIV and considered to generate the acceleration unbalance between both vortex layers that induces the jet wavy motion coupled with the pipe resonance. Vortices from the jet visualized by direct numerical simulations are briefly discussed.

Highlights

  • Musical wind instruments have a mechanism converting the direct energy of the fluid flow into the alternative energy of the sound

  • Vortices on sound generation are clearly revealed in edge tones and cavity tones

  • Relatively large vortices are seen in flue instruments driven by thick jets, these are in rare cases

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Summary

Introduction

Musical wind instruments have a mechanism converting the direct energy of the fluid flow into the alternative energy of the sound. Howe [18] assumes that a compact vortex core with relatively large size appearing alternately just above and below the pipe edge is created by the interaction between the jet velocity vector U and the cross-flow velocity (acoustic reciprocating velocity) vector u at the mouth opening formed between the flue and the edge This vortex core with the vorticity ω ð1⁄4 ∇ Â UÞ is considered to drive the air column in the pipe. The sound excitation by this periodic vortex shedding at the edge is controlled by the product of the aeroacoustic source term div ðω Â UÞ and the potential function representing the irrotational cross-flow u at the mouth This discrete-vortex model of Howe is successfully applied to analyze and evaluate both cavity-tone generation [9] and tone generation in flue instruments [10, 14] when the jet is thick and the condition d/h < 2 (d the width of the mouth opening or the flue-to-edge distance and h the jet thickness) is satisfied.

Jet-drive model
Jet wave and its amplification
Jet-drive model for large jet displacements
Discrete-vortex model based on the vortex shedding at the edge
Discrete-vortex model based on the vortex shedding at the flue exit
Flow visualization and some discussion
Feedback loop gain and time delay of the jet wave in the jet-drive model
Time delay of vortex convection in the discrete-vortex model
Aspect ratio d/h of the jet
Vortex-layer model
Sound dissipations in linear acoustics
Sound dissipation at the internal wall of a long pipe
Finite cylindrical pipe: acoustic resonance and sound radiation
Acoustically induced vortices as the final dissipation agent
Visualization of acoustic vortices and their modeling
Acoustic power balance between vortex layers and acoustic vortices
Acoustic losses due to vortex shedding at the edge
Vortices on sound generation
Vortex layer along the jet visualized by PIV
Measurement requirements
Measurement procedures
Calculation of the acoustic generation formula
Dominant area for the acoustic power generation and receptivity problem
Vortices from the jet visualized by direct numerical simulations
Findings
Conclusions

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