Rotor broadband noise due to surface roughness during ice accretion

Baofeng Cheng, Yiqiang Han, Kenneth Steven Brentner, Jose Palacios, Philip John Morris, David Hanson, Michael P. Kinzel

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

2 Citations (Scopus)

Abstract

The change of helicopter rotor broadband noise due to different surface roughness during ice accretion is investigated. Comprehensive rotor broadband noise measurements are carried out on rotor blades with different roughness sizes and rotation speeds in two facilities: the Adverse Environment Rotor Test Stand (AERTS) facility at The Pennsylvania State University, and the University of Maryland Acoustic Chamber (UMAC). In both facilities the measured high-frequency broadband noise increases significantly with increasing surface roughness heights. Rotor broadband noise source identification is conducted and the broadband noise related to ice accretion is thought to be turbulent boundary layer trailing edge (TBL-TE) noise. Theory suggests TBL-TE noise scales with Mach number to the fifth power, which is also observed in the experimental data – confirming that the dominant broadband noise mechanism during ice accretion is trailing edge noise. The trailing edge noise theories developed by Ffowcs Williams and Hall, and Howe both identify two important parameters: boundary layer thickness and turbulence intensity. Numerical studies of 2-D airfoils with different ice-induced surface roughness heights are conducted to investigate the extent that surface roughness impacts the boundary layer thickness and turbulence intensity (and ultimately the TBL-TE noise). The results show that boundary layer thickness and turbulence intensity at the trailing edge increase with the increased roughness height. Using Howe’s trailing edge noise model, the increased sound pressure level (SPL) of the trailing edge noise due to the increased displacement thickness and normalized integrated turbulence intensity are 6.2 dB and 1.6 dB for large and small accreted ice roughness heights, respectively. The estimated increased SPL values agree reasonably well with the experimental results, which are 5.8 dB and 2.6 dB for large and small roughness height, respectively.

Original languageEnglish (US)
Title of host publication54th AIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103933
StatePublished - Jan 1 2016
Event54th AIAA Aerospace Sciences Meeting, 2016 - San Diego, United States
Duration: Jan 4 2016Jan 8 2016

Publication series

Name54th AIAA Aerospace Sciences Meeting

Other

Other54th AIAA Aerospace Sciences Meeting, 2016
CountryUnited States
CitySan Diego
Period1/4/161/8/16

Fingerprint

Ice
Rotors
Surface roughness
Boundary layers
Turbulence
Acoustic waves
Helicopter rotors
Airfoils
Acoustic noise
Mach number
Turbomachine blades
Acoustics

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Cite this

Cheng, B., Han, Y., Brentner, K. S., Palacios, J., Morris, P. J., Hanson, D., & Kinzel, M. P. (2016). Rotor broadband noise due to surface roughness during ice accretion. In 54th AIAA Aerospace Sciences Meeting (54th AIAA Aerospace Sciences Meeting). American Institute of Aeronautics and Astronautics Inc, AIAA.
Cheng, Baofeng ; Han, Yiqiang ; Brentner, Kenneth Steven ; Palacios, Jose ; Morris, Philip John ; Hanson, David ; Kinzel, Michael P. / Rotor broadband noise due to surface roughness during ice accretion. 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (54th AIAA Aerospace Sciences Meeting).
@inproceedings{9a1369476c334dd4a8942a67b73b465b,
title = "Rotor broadband noise due to surface roughness during ice accretion",
abstract = "The change of helicopter rotor broadband noise due to different surface roughness during ice accretion is investigated. Comprehensive rotor broadband noise measurements are carried out on rotor blades with different roughness sizes and rotation speeds in two facilities: the Adverse Environment Rotor Test Stand (AERTS) facility at The Pennsylvania State University, and the University of Maryland Acoustic Chamber (UMAC). In both facilities the measured high-frequency broadband noise increases significantly with increasing surface roughness heights. Rotor broadband noise source identification is conducted and the broadband noise related to ice accretion is thought to be turbulent boundary layer trailing edge (TBL-TE) noise. Theory suggests TBL-TE noise scales with Mach number to the fifth power, which is also observed in the experimental data – confirming that the dominant broadband noise mechanism during ice accretion is trailing edge noise. The trailing edge noise theories developed by Ffowcs Williams and Hall, and Howe both identify two important parameters: boundary layer thickness and turbulence intensity. Numerical studies of 2-D airfoils with different ice-induced surface roughness heights are conducted to investigate the extent that surface roughness impacts the boundary layer thickness and turbulence intensity (and ultimately the TBL-TE noise). The results show that boundary layer thickness and turbulence intensity at the trailing edge increase with the increased roughness height. Using Howe’s trailing edge noise model, the increased sound pressure level (SPL) of the trailing edge noise due to the increased displacement thickness and normalized integrated turbulence intensity are 6.2 dB and 1.6 dB for large and small accreted ice roughness heights, respectively. The estimated increased SPL values agree reasonably well with the experimental results, which are 5.8 dB and 2.6 dB for large and small roughness height, respectively.",
author = "Baofeng Cheng and Yiqiang Han and Brentner, {Kenneth Steven} and Jose Palacios and Morris, {Philip John} and David Hanson and Kinzel, {Michael P.}",
year = "2016",
month = "1",
day = "1",
language = "English (US)",
isbn = "9781624103933",
series = "54th AIAA Aerospace Sciences Meeting",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "54th AIAA Aerospace Sciences Meeting",

}

Cheng, B, Han, Y, Brentner, KS, Palacios, J, Morris, PJ, Hanson, D & Kinzel, MP 2016, Rotor broadband noise due to surface roughness during ice accretion. in 54th AIAA Aerospace Sciences Meeting. 54th AIAA Aerospace Sciences Meeting, American Institute of Aeronautics and Astronautics Inc, AIAA, 54th AIAA Aerospace Sciences Meeting, 2016, San Diego, United States, 1/4/16.

Rotor broadband noise due to surface roughness during ice accretion. / Cheng, Baofeng; Han, Yiqiang; Brentner, Kenneth Steven; Palacios, Jose; Morris, Philip John; Hanson, David; Kinzel, Michael P.

54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016. (54th AIAA Aerospace Sciences Meeting).

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

TY - GEN

T1 - Rotor broadband noise due to surface roughness during ice accretion

AU - Cheng, Baofeng

AU - Han, Yiqiang

AU - Brentner, Kenneth Steven

AU - Palacios, Jose

AU - Morris, Philip John

AU - Hanson, David

AU - Kinzel, Michael P.

PY - 2016/1/1

Y1 - 2016/1/1

N2 - The change of helicopter rotor broadband noise due to different surface roughness during ice accretion is investigated. Comprehensive rotor broadband noise measurements are carried out on rotor blades with different roughness sizes and rotation speeds in two facilities: the Adverse Environment Rotor Test Stand (AERTS) facility at The Pennsylvania State University, and the University of Maryland Acoustic Chamber (UMAC). In both facilities the measured high-frequency broadband noise increases significantly with increasing surface roughness heights. Rotor broadband noise source identification is conducted and the broadband noise related to ice accretion is thought to be turbulent boundary layer trailing edge (TBL-TE) noise. Theory suggests TBL-TE noise scales with Mach number to the fifth power, which is also observed in the experimental data – confirming that the dominant broadband noise mechanism during ice accretion is trailing edge noise. The trailing edge noise theories developed by Ffowcs Williams and Hall, and Howe both identify two important parameters: boundary layer thickness and turbulence intensity. Numerical studies of 2-D airfoils with different ice-induced surface roughness heights are conducted to investigate the extent that surface roughness impacts the boundary layer thickness and turbulence intensity (and ultimately the TBL-TE noise). The results show that boundary layer thickness and turbulence intensity at the trailing edge increase with the increased roughness height. Using Howe’s trailing edge noise model, the increased sound pressure level (SPL) of the trailing edge noise due to the increased displacement thickness and normalized integrated turbulence intensity are 6.2 dB and 1.6 dB for large and small accreted ice roughness heights, respectively. The estimated increased SPL values agree reasonably well with the experimental results, which are 5.8 dB and 2.6 dB for large and small roughness height, respectively.

AB - The change of helicopter rotor broadband noise due to different surface roughness during ice accretion is investigated. Comprehensive rotor broadband noise measurements are carried out on rotor blades with different roughness sizes and rotation speeds in two facilities: the Adverse Environment Rotor Test Stand (AERTS) facility at The Pennsylvania State University, and the University of Maryland Acoustic Chamber (UMAC). In both facilities the measured high-frequency broadband noise increases significantly with increasing surface roughness heights. Rotor broadband noise source identification is conducted and the broadband noise related to ice accretion is thought to be turbulent boundary layer trailing edge (TBL-TE) noise. Theory suggests TBL-TE noise scales with Mach number to the fifth power, which is also observed in the experimental data – confirming that the dominant broadband noise mechanism during ice accretion is trailing edge noise. The trailing edge noise theories developed by Ffowcs Williams and Hall, and Howe both identify two important parameters: boundary layer thickness and turbulence intensity. Numerical studies of 2-D airfoils with different ice-induced surface roughness heights are conducted to investigate the extent that surface roughness impacts the boundary layer thickness and turbulence intensity (and ultimately the TBL-TE noise). The results show that boundary layer thickness and turbulence intensity at the trailing edge increase with the increased roughness height. Using Howe’s trailing edge noise model, the increased sound pressure level (SPL) of the trailing edge noise due to the increased displacement thickness and normalized integrated turbulence intensity are 6.2 dB and 1.6 dB for large and small accreted ice roughness heights, respectively. The estimated increased SPL values agree reasonably well with the experimental results, which are 5.8 dB and 2.6 dB for large and small roughness height, respectively.

UR - http://www.scopus.com/inward/record.url?scp=84980392817&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84980392817&partnerID=8YFLogxK

M3 - Conference contribution

SN - 9781624103933

T3 - 54th AIAA Aerospace Sciences Meeting

BT - 54th AIAA Aerospace Sciences Meeting

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

ER -

Cheng B, Han Y, Brentner KS, Palacios J, Morris PJ, Hanson D et al. Rotor broadband noise due to surface roughness during ice accretion. In 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA. 2016. (54th AIAA Aerospace Sciences Meeting).