Simulation of powered resonance tubes: Understanding parameter space

A. B. Cain, Edward J Kerschen, G. Raman, S. Sarpotdar

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

New simulations of powered resonance tubes (PRT) have been performed at two Reynolds numbers that differ by a factor of 10. The lower Reynolds results show strong regularity with some disorder showing up in the higher Reynolds number cases. Remarkably the simulations show that the dominant frequencies, amplitude and directivity of the PRT actuator output field are largely unaffected by the factor of 10 increase in Reynolds number considered here. However, the increase in Reynolds number is shown to substantially affect the width of the resonance peaks, and the vorticity distributions and flow details more generally. The effort to integrate simulations, theory, and experiment has been fruitful. There is general agreement between these three methods in terms of the frequency, amplitude, and directivity of the actuator output field, to the extent that they have been examined.

Original languageEnglish (US)
Title of host publication9th AIAA/CEAS Aeroacoustics Conference and Exhibit
StatePublished - 2003
Event9th AIAA/CEAS Aeroacoustics Conference and Exhibit, 2003 - Hilton Head, SC, United States
Duration: May 12 2003May 14 2003

Other

Other9th AIAA/CEAS Aeroacoustics Conference and Exhibit, 2003
CountryUnited States
CityHilton Head, SC
Period5/12/035/14/03

Fingerprint

Reynolds number
directivity
tubes
actuators
Actuators
simulation
output
high Reynolds number
regularity
vorticity
Vorticity
disorders
Experiments

ASJC Scopus subject areas

  • Aerospace Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering
  • Acoustics and Ultrasonics

Cite this

Cain, A. B., Kerschen, E. J., Raman, G., & Sarpotdar, S. (2003). Simulation of powered resonance tubes: Understanding parameter space. In 9th AIAA/CEAS Aeroacoustics Conference and Exhibit

Simulation of powered resonance tubes : Understanding parameter space. / Cain, A. B.; Kerschen, Edward J; Raman, G.; Sarpotdar, S.

9th AIAA/CEAS Aeroacoustics Conference and Exhibit. 2003.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Cain, AB, Kerschen, EJ, Raman, G & Sarpotdar, S 2003, Simulation of powered resonance tubes: Understanding parameter space. in 9th AIAA/CEAS Aeroacoustics Conference and Exhibit. 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, 2003, Hilton Head, SC, United States, 5/12/03.
Cain AB, Kerschen EJ, Raman G, Sarpotdar S. Simulation of powered resonance tubes: Understanding parameter space. In 9th AIAA/CEAS Aeroacoustics Conference and Exhibit. 2003
Cain, A. B. ; Kerschen, Edward J ; Raman, G. ; Sarpotdar, S. / Simulation of powered resonance tubes : Understanding parameter space. 9th AIAA/CEAS Aeroacoustics Conference and Exhibit. 2003.
@inproceedings{21a42ad15e7843e7bac8ad6ae2553338,
title = "Simulation of powered resonance tubes: Understanding parameter space",
abstract = "New simulations of powered resonance tubes (PRT) have been performed at two Reynolds numbers that differ by a factor of 10. The lower Reynolds results show strong regularity with some disorder showing up in the higher Reynolds number cases. Remarkably the simulations show that the dominant frequencies, amplitude and directivity of the PRT actuator output field are largely unaffected by the factor of 10 increase in Reynolds number considered here. However, the increase in Reynolds number is shown to substantially affect the width of the resonance peaks, and the vorticity distributions and flow details more generally. The effort to integrate simulations, theory, and experiment has been fruitful. There is general agreement between these three methods in terms of the frequency, amplitude, and directivity of the actuator output field, to the extent that they have been examined.",
author = "Cain, {A. B.} and Kerschen, {Edward J} and G. Raman and S. Sarpotdar",
year = "2003",
language = "English (US)",
isbn = "9781624101021",
booktitle = "9th AIAA/CEAS Aeroacoustics Conference and Exhibit",

}

TY - GEN

T1 - Simulation of powered resonance tubes

T2 - Understanding parameter space

AU - Cain, A. B.

AU - Kerschen, Edward J

AU - Raman, G.

AU - Sarpotdar, S.

PY - 2003

Y1 - 2003

N2 - New simulations of powered resonance tubes (PRT) have been performed at two Reynolds numbers that differ by a factor of 10. The lower Reynolds results show strong regularity with some disorder showing up in the higher Reynolds number cases. Remarkably the simulations show that the dominant frequencies, amplitude and directivity of the PRT actuator output field are largely unaffected by the factor of 10 increase in Reynolds number considered here. However, the increase in Reynolds number is shown to substantially affect the width of the resonance peaks, and the vorticity distributions and flow details more generally. The effort to integrate simulations, theory, and experiment has been fruitful. There is general agreement between these three methods in terms of the frequency, amplitude, and directivity of the actuator output field, to the extent that they have been examined.

AB - New simulations of powered resonance tubes (PRT) have been performed at two Reynolds numbers that differ by a factor of 10. The lower Reynolds results show strong regularity with some disorder showing up in the higher Reynolds number cases. Remarkably the simulations show that the dominant frequencies, amplitude and directivity of the PRT actuator output field are largely unaffected by the factor of 10 increase in Reynolds number considered here. However, the increase in Reynolds number is shown to substantially affect the width of the resonance peaks, and the vorticity distributions and flow details more generally. The effort to integrate simulations, theory, and experiment has been fruitful. There is general agreement between these three methods in terms of the frequency, amplitude, and directivity of the actuator output field, to the extent that they have been examined.

UR - http://www.scopus.com/inward/record.url?scp=84894553693&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84894553693&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84894553693

SN - 9781624101021

BT - 9th AIAA/CEAS Aeroacoustics Conference and Exhibit

ER -