Technical Papers
Oct 12, 2012

NASA Glenn’s Contributions to Aircraft Engine Noise Research

Publication: Journal of Aerospace Engineering
Volume 26, Issue 2

Abstract

This paper reviews all engine noise research conducted at the National Aeronautics and Space Administration (NASA) Glenn Research Center over the last 70 years. The review includes a historical perspective of the center and the facilities used to conduct the research. Major NASA noise research programs are highlighted, showing their impact on the industry and on the development of aircraft noise reduction technology. Noise reduction trends are discussed, and future aircraft concepts are presented. Results show that, since the 1960s, the average perceived noise level has been reduced by about 20 dB. Studies show that, depending on the size of the airport, the aircraft fleet mix, and the actual growth in air travel, another 15–17 dB is required to achieve NASA’s long-term goal of providing technologies to limit objectionable noise to the boundaries of an average airport.

Get full access to this article

View all available purchase options and get full access to this article.

Acknowledgments

Thanks goes to the hundreds of people at NASA Glenn Research Center that since the early 1950s have dedicated their professional careers to improving the quality of life near the world’s airports by developing technologies for reducing engine noise. What is often not obvious to the general public is the amount of time it takes to conduct tests across multiple shifts over long periods of time (months to years) without a break. The dedication of the test teams comes with a sacrifice to their personal lives and families. The analytical work has attracted the finest theoreticians in the world to either work directly at the center or to visit the center to collaborate on cutting edge research. Thanks also go to the academic and industry partners who have helped NASA advance and utilize the state of the art technologies in their products.

References

Abdalla, K. L., and Yuska, J. A. (1975). “NASA REFAN program status.” Rep. TM X–71705, NASA, Cleveland.
Beranek, L. (2008). “Bolt Beranek & Newman, the United Nations, Big Noise, and the Internet.” Chapter 5, Riding the waves, MIT Press, Cambridge, MA, 107–109.
Bowles, M. D. (2010). “The ‘apollo’ of aeronautics, NASA's aircraft energy efficiency program 1973–1987.” Rep. SP–2009–574, NASA, Washington, DC.
Bradley, M. K., and Droney, C. K. (2011). “Subsonic ultra green aircraft research, Phase 1 final report.” Rep. CR–2011-216847, NASA, Hampton, VA.
Bridges, J., and Brown, C. A. (2004). “Parametric testing of chevrons on single flow hot jets.” Rep. TM—2004-213107, NASA, Cleveland.
Bridges, J., and Wernet, M. (2004). “Measurements of aeroacoustic sound source in hot jets.” Rep. TM—2004-212508, NASA, Cleveland.
Bridges, J. E., et al. (2012). “Jet noise prediction.” Chapter 8, Assessment of NASA’s aircraft noise prediction Capability, M. D. Dahl, ed., NASA, Cleveland, 278–285.
Brown, C. A. (2008). “Scalability of localized arc filament plasma actuators.” Rep. TM—2008-215278, NASA, Cleveland.
Bruner, S., et al. (2010). “NASA N+3 subsonic fixed wing silent efficient low-emissions commercial transport (SELECT) vehicle study.” Rep. CR—2010-216798, NASA, Hampton, VA.
Burleson, C. E. (2007). “Aviation and the environment—Managing the challenge of growth.” Fund. Aeronaut. Prog. Ann. Meet., NASA, New Orleans, 3.
Ciepluch, C. C. (1975). “A review of the QCSEE program.” Rep. TM X–71818, NASA, Cleveland.
Ciepluch, C. C., et al. (1958). “Acoustics, thrust, and drag characteristics of several full scale noise suppressors for turbojet engines.” Rep. TN 4261, NASA, Cleveland.
Coles, W. D. (1959). “Jet-engine exhaust noise from slot nozzles.” Rep. TN–D–60, NASA, Cleveland.
Dahl, M., ed. (2000). “Third computational aeroacoustic (CAA) workshop on benchmark problems.” Rep. CP—2000-209790, NASA, Cleveland.
Dahl, M. D., ed. (2004). “Fourth computational aeroacoustics (CAA) workshop on benchmark problems.” Rep. CP—2004-212954, NASA, Cleveland.
Dalton, W. N., III. (2003). “Ultra high bypass ratio low noise engine study.” Rep. CR—2003-212523, NASA, Cleveland.
D'Angelo, M. M., et al. (2010). “N+3 small commercial efficient and quiet transportation for year 2030–2035.” Rep. CR—2010-216691, NASA, Hampton, VA.
Davis, D. D. (1957). “Acoustical filters and mufflers.” Handbook of noise control, C. M. Harris, ed., McGraw Hill, New York, 21–40.
Dawson, V. P. (1991). “Engines and innovation.” Rep. SP–4306, NASA, Washington, DC.
Dittmar, J. D., et al. (2003). “The noise of a forward swept fan.” Rep. TM—2003-212208, NASA, Cleveland.
Dittmar, J. H., et al. (1999). “Some acoustic results from the Pratt & Whitney advanced ducted propulsor—Fan 1.” Rep. TM—1999-209049, NASA, Cleveland.
Dittmar, J. H., et al. (2000). “The alternative low noise fan.” Rep. TM—2000-209916, NASA, Cleveland.
Dittmar, J. H., Woodward, R. P., and MacKinnon, M. J. (1984). “Fan noise reduction achieved by removing tip flow irregularities behind the rotor—Forward arc test configuration.” Rep. TM–83616, NASA, Cleveland.
Dorsch, R. G., Krejsa, E. A., and Olsen, W. A. (1971). “Blown flap noise research.” Rep. TM X–67850, NASA, Cleveland.
Dougherty, R. P., et al. (2010). “Locating and quantifying broadband sources using in-duct microphones.” Rep. TM—2010-216931, NASA, Cleveland.
Elliott, D. M. (2010). “Acoustic performance of novel fan noise reduction technologies for a high bypass model turbofan at simulated flight conditions.” Rep. TM—2010-215841, NASA, Cleveland.
Envia, E. (2002). “Fan noise source diagnostics test—Vane unsteady pressure results.” Rep. TM—2002-211808, NASA, Cleveland.
Envia, E., et al. (2012). “Fan noise prediction.” Chapter 5, Assessment of NASA’s aircraft noise prediction capability, M. D. Dahl, ed., NASA, Cleveland, 137.
Envia, E., and Nallasamy, M. (1998). “Design selection and analysis of a swept and leaned stator concept.” Rep. TM—1998-208662, NASA, Cleveland.
Feiler, C. E., and Groeneweg, J. F. (1977). “Summary of forward velocity effects on fan noise.” Rep. TM–73722, NASA, Cleveland.
Felder, J. L., et al. (2011). “Turboelectic distributed propulsion in a hybrid wing body aircraft.” Rep. ISABE–2011–1340, American Institute of Aeronautics and Astronautics, Gothenburg, Sweden.
Fite, E. B. (2006). “Fan performance from duct rake instrumentation on a 1.294 pressure ratio, 725 ft/sec tip speed turbofan simulator using vaned passage casing treatment.” Rep. TM—2006-214241, NASA, Cleveland.
German, J., et al. (1981). “Design and evaluation of an intregrated quiet clean general aviation turbofan (QCGAT) engine and aircraft propulsion system.” Rep. CR–165185, NASA, Cleveland.
Gliebe, P. R., and Janardan, B. A. (2003). “Ultra-high bypass engine aeroacoustic study.” Rep. CR—2003-212525, NASA, Cleveland.
Goldstein, M. E. (1974). “Aeroacoustics.” Rep. SP–346, NASA, Cleveland.
Greitzer, E. M., et al. (2010). “N+3 aircraft concept designs and trade studies, final report volumes 1 and 2.” Rep. CR—2010-216794, NASA, Hampton, VA.
Groeneweg, J. F., et al. (1991). “Turbomachinery noise.” Acoustics of flight vehicles: Theory and practice, H. H. Hubbard, ed., Vol. 1, NASA, Hampton, VA, 166.
Guynn, M. D., et al. (2011). “Refined exploration of turbofan design options for an advanced single-aisle transport.” Rep. TM—2011-216883, NASA, Hampton, VA.
Hager, R. D., and Vrabel, D. (1988). “Advanced turboprop project.” Rep. SP–495, NASA, Washington, DC.
Hayden, R. E., et al. (1977). “Analysis and design of a high speed, low noise aircraft fan incorporating swept leading edge rotor and stator blades.” Rep. CR–135092, NASA, Cleveland.
Heidelberg, L. J. (2002). “Fan noise source diagnostics test—Tone modal structure results.” Rep. TM—2002-211594, NASA, Cleveland.
Heidmann, M. F. (1979). “Interim prediction method for fan and compressor source noise.” Rep. TM X–71763, NASA, Cleveland.
Henderson, B. (2010). “Fifty years of fluidic injection for jet noise reduction.” Int. J. of Aeroacoustics, 9(1–2), 91–122.
Henderson, B. (2012). “Aeroacoustics of three-stream jets.” Rep. 2012–2159, American Institute of Aeronautics and Astronautics, Reston, VA.
Hildenbrand, R., and Norgren, W. M. (1980). “AiResearch QCGAT program final report.” Rep. CR–159758, NASA, Cleveland.
Holcombe, V. (2003). “Aero-propulsion technology (APT), Task V low noise ADP engine definition study.” Rep. CR—2003-212521, NASA, Cleveland.
Howes, W. L., et al. (1957). “Near field noise of a jet-engine exhaust.” Rep. 1338, NASA, Cleveland.
Huff, D. L., and Gliebe, P. (2003). “Recent progress in engine noise reduction technologies.” Proc., 41st AIAA Aero. Sci. Meet., American Institute of Aeronautics and Astronautics, Reston, VA, 63.
Huff, R. G., et al. (1974). “Interim prediction method for low frequency core engine noise.” Rep. TM X–71627, NASA, Cleveland.
Hughes, C. E., et al. (2005). “Fan noise source diagnostic test—Rotor alone aerodynamic performance results.” Rep. TM—2002-211681, NASA, Cleveland.
International Civil Aviation Organization (ICAO). (2004). “ICAO/CAEP current activities on noise certification.” Noise Certification Workshop, 〈http://legacy.icao.int/icao/en/atb/atbworkshops/2004/noisecertificationworkshop_04/Presentations/BIP_5tc.pdf〉 (Jul. 3, 2012).
Jeracki, R. J. (2006). “Comprehensive report of fan performance from duct rake instrumentation on 1.294 pressure ratio, 806 ft/sec tip speed turbofan simulator models.” Rep. TM—2006-213863, NASA, Cleveland.
Khavaran, A., et al. (2005). “Prediction of turbulence-generated noise in unheated jets; part 1: JeNo technical manual (version 1.0).” Rep. TM—2005-213827, NASA, Cleveland.
Koenig, R. W., and Sievers, G. K. (1979). “Preliminary QCGAT program test results.” Rep. TM–79013, NASA, Cleveland.
Kontos, K. B., et al. (1996). “Improved NASA–ANOPP noise prediction computer code for advanced subsonic propulsion systems.” Rep. CR–195480, NASA, Cleveland.
Kramer, J. J., and Montegani, F. J. (1972). “The NASA quiet engine program.” Rep. TM X–67988, NASA, Cleveland.
Krejsa, E. A., and Valerino, M. F. (1976). “Interim prediction method for turbine noise.” Rep. TM X–73566, NASA, Cleveland.
Kumasaka, H. A., et al. (1996). “Definition of 1992 technology aircraft noise levels and the methodology for addressing airplane noise impact of component noise reduction concepts.” Rep. CR–198298, NASA, Hampton, VA.
Lee, S. S., and Bridges, J. (2005). “Phased-array measurements of single flow hot jets.” Rep. TM—2005-213826, NASA, Cleveland.
Lieber, L., et al. (1996). “Quiet high-speed fan.” Rep. CR–198518, NASA, Cleveland.
Lighthill, M. J. (1952). “On sound generated aerodynamically. I. General theory.” Proc. R. Soc. Lond. A Math. Phys. Sci., 211(1107), 564–587. doi:10.1098/rspa.1952.0060
Lighthill, M. J. (1954). “On sound generated aerodynamically. II. Turbulence as a source of sound.” Proc. R. Soc. Lond. A Math. Phys. Sci., 222(1148), 1–32.doi:10.1098/rspa.1954.0049
Miles, J. H. (2008). “Spectral separation of the turbofan engine coherent combustion noise component.” Rep. TM—2008-215157, NASA, Cleveland.
Nallasamy, M., and Envia, E. (2005). “Computation of rotor wake turbulence noise.” J. Sound Vibrat., 282(3–5), 649–678. doi:10.1016/j.jsv.2004.03.062
Ohio Aerospace Institute (OAI). (2008). “The challenge.” Aeroacoustic Research Consortium, 〈http://www.oai.org/aeroacoustics/challenge.html〉 (Feb. 24, 2012).
Podboy, G. G., et al. (2003). “Fan noise source diagnostic test—LDV measured flow field results.” Rep. TM—2003-212330, NASA, Cleveland.
Repp, R., et al. (2003). “Design and test of a fan/nacelle models of a high-speed fan design.” Rep. CR—2003-212369, NASA, Cleveland.
Rice, E. J. (1976). “Acoustic liner optimum impedance for spinning modes with mode cut-off ratio as a design criterion.” Rep. TM X–73411, NASA, Cleveland.
Rice, E. J. (1977). “Multimodal far-field acoustic radiation pattern—An approximate equation.” Rep. TM–73721, NASA, Cleveland.
Sams, E. W., and Bresnahan, D. L. (1973). “REFAN program, Phase I—Summary report.” Rep. TM X–71456, NASA, Cleveland.
Saule, A. V. (1976). “Modal structure inferred from static engine far-field noise directivity.” Rep. TM X–71909, NASA, Cleveland.
Shovlin, M. D., and Cochrane, J. A. (1978). “An overview of the quiet short-haul research aircraft program.” Rep. TM 78545, NASA, Moffett Field, CA.
Sokhey, J. S. (2012). “N+2 low noise exhaust nozzle validation—RRLW mixer-ejector concept.” Proc., Fund. Aero. Prog. Conf., NASA, Washington, DC, 5.
Stitt, L. E. (1990). “Exhaust nozzles for propulsion systems with emphasis on supersonic cruise aircraft.” Rep. RP–1235, NASA, Cleveland.
Stone, J. (1974). “Interim prediction method for jet noise.” Rep. TM X–71618, NASA, Cleveland.
Stone, J. R. (1977). “An empirical model for inverted-velocity-profile jet noise prediction.” Rep. TM–73838, NASA, Cleveland.
Stone, J. R., et al. (2009). “Jet noise modeling for supressed and unsupressed aircraft in simulated flight.” Rep. TM—2009-215524, NASA, Cleveland.
Sutliff, D. L. (2005). “Broadband noise reduction of a low-speed fan using trailing edge blowing.” Rep. TM—2005-213814, NASA, Cleveland.
Sutliff, D. L., et al. (2009). “Attenuation of FJ44 turbofan engine noise with a foam-metal liner installed over the rotor.” Rep. TM—2009-215666, NASA, Cleveland.
Thomas, R. H., et al. (2010). “Hybrid wing body aircraft system noise assessment with propulsion airframe aeroacoustic experiments.” Rep. 2010–3913, American Institute of Aeronautics and Astronautics, Hampton, VA.
U.S. Environmental Protection Agency, Office of Noise Abatement and Control. (1974). “Information on levels of environmental noise requisite to protect public health and welfare with an adequate margin of safety.” Rep. 550/9–74–004, Environmental Protection Agency, Washington, DC.
Vance, T. (1987). “NASA Ames Research Center—QSRA Research Aircraft at NAS Moffett Field '87.” Youtube, 〈http://www.youtube.com/watch?v=_4QiW-ROJtg〉 (Feb. 23, 2012).
Weir, D. (2003). “Design and test of fan/nacelle models quiet high-speed fan.” Rep. CR–212370, NASA, Cleveland.
Weir, D. (2004). “Engine validation of noise reduction concepts—Separate flow nozzles.” Rep. 2004–0188, American Institute of Aeronautics and Astronautics, Reston, VA.
Weir, D., ed. (2008). “Engine validation of noise and emission reduction technology phase I.” Rep. CR—2008-215225, NASA, Cleveland.
Weir, D., Bouldin, B., and Mendoza, J. (2006). “Static and flight aeroacoustic evaluations of a scarf inlet.” Rep. 2006–2462, American Institute of Aeronautics and Astronautics, Reston, VA.
Weir, D., and Mendoza, J. (2005). “Static and flight aeroacoustic evaluations of a variable exhaust nozzle.” Rep. 2005–3049, American Institute of Aeronautics and Astronautics, Reston, VA.
Weir, D., and Podboy, G. (2005). “Flow measurements and multiple pure tone noise from a forward swept fan.” Rep. 2005–1200, American Institute of Aeronautics and Astronautics, Reston, VA.
Woodward, R., et al. (1998). “Benefits of swept and leaned stators for fan noise reduction.” Rep. TM—1998-208661, NASA, Cleveland.
Woodward, R. P., et al. (2002). “Fan noise source diagnostic test—Far field acoustic results.” Rep. TM—2002-211591, NASA, Cleveland.
Woodward, R. P., et al. (2007). “Noise benefits of rotor trailing edge blowing for a model turbofan.” Rep. TM—2007-214666, NASA, Cleveland.
Woodward, R. P., and Hughes, C. E. (2005). “Noise benefits of increased fan bypass nozzle area.” Rep. 2005–1201, American Institute of Aeronautics and Astronautics, Reno, NV.
Zaman, K. B. M. Q., et al. (2011). Evolution from ‘tabs' to ‘chevron technology'—A review, Vol. 10, Multi-Science, Brentwood, U.K.

Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 26Issue 2April 2013
Pages: 218 - 250

History

Received: Mar 30, 2012
Accepted: Oct 10, 2012
Published online: Oct 12, 2012
Published in print: Apr 1, 2013

Permissions

Request permissions for this article.

Authors

Affiliations

Dennis L. Huff [email protected]
Deputy Chief, Aeropropulsion Division, National Aeronautics and Space Administration Glenn Research Center, 21000 Brookpark Rd., Cleveland, OH 44135. E-mail: [email protected]

Metrics & Citations

Metrics

Citations

Download citation

If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.

Cited by

View Options

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Media

Figures

Other

Tables

Share

Share

Copy the content Link

Share with email

Email a colleague

Share