Investigation All Types of Aircraft Noises: Review Paper
American Journal of Science, Engineering and Technology
Volume 5, Issue 1, March 2020, Pages: 33-41
Received: Jan. 8, 2020; Accepted: Mar. 2, 2020; Published: Mar. 10, 2020
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Mojtaba Sadeghian, School of Mechanical Engineering, Babol Noshirvani University of Technology, Babol, Iran
Mofid Gorji-Bandpy, Faculty of Mechanical Engineering, Noshirvani University of Technology, Babol, Iran
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This article presents a review of current aircraft noises. Noise is a fascinating area of research combining statistics, applied mathematics, and engineering. Aircraft noises are an impact of enormous financial, environmental, and technological issue. Aircraft noise remains the key inhibitor of the growth of air transportation and remains an acute environmental problem that requires advanced solutions. To advance our understanding of the sound source mechanisms, it should be noted that predominant noise sources of aircraft engines are from the exhaust (referred to as the jet) and fan (including the stator). The noise generated in these two areas during takeoff and landing has a strong influence on the communities around the airports. One of the most important sources of aircraft noises in modern jet aircraft is the turbulence that occurs in the shear layers around the engine’s exhaust. But this is not just an academic issue also jet noise is highly relevant to the aviation industry and on a wider scale, has been related to economic, social, and subsequently political. To deal with this problem, aircraft manufacturers and public establishments are engaged in research on technical and theoretical approaches for noise reduction concepts that should be applied to new aircraft. This review paper discusses a selection of enabling technologies and their implications on acoustics and noise and gives a perspective on future trends and new directions in aeroacoustics required to address the challenges.
Aircraft Noise, Landing Gear Noise, Technology Trends, Aero Acoustics, Airframe Noise, Fan Noise, Jet Noise
To cite this article
Mojtaba Sadeghian, Mofid Gorji-Bandpy, Investigation All Types of Aircraft Noises: Review Paper, American Journal of Science, Engineering and Technology. Vol. 5, No. 1, 2020, pp. 33-41. doi: 10.11648/j.ajset.20200501.14
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This article is an open access article distributed under the Creative Commons Attribution License ( which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
D. G. Crighton Chapter on Airframe Noise in Aero acoustics of Flight vehicles: theory and Practice: Noise Sources. NASA Reference Publication 90-3052 (H. H. Hubbard, editor) 1991.
M. R. Fink FAA-RD-77-29, Airframe noise prediction, 1977.
Heller H, Dobrzynski W, Sound radiation from aircraft wheel-well/landing gear configurations, Journal of Aircraft, vol. 14, no. 8, pp. 768-774, August 1977.
Hubbard H, Aero acoustics of flight vehicles: theory and practice, volume 1: noise sources, in: Crighton: D. (Ed.), Airframe noise, pp. 391-447, NASA RP- 1258. 1991.
Hayes H, W. Horne, Paul Soderman, Airframe noise characteristics of a 4.7% DC 10 model, AIAA-97-1594.
Blackner A. M, Davis C. M, Airframe noise source identification using elliptical mirror measurement techniques, Proceedings of Inter-Noise 95, pp. 203-206, Newport Beach, CA, USA, 70 - 12 July 1995.
Dobrzynski Wet al, Full scale noise testing on Airbus landing gears in German Dutch wind tunnel, AIAA-97-1597.
Piet J et al, airframe noise source localization using a microphone array, AIAA-97.1643.
Dobrzynski W et. al, Airframe Noise Studies on Wings with Deployed High Lift Devices, IAA/CEAS-98-2337. 1998.
Werner Dobrzynski, Burkhard Gehlhar, Heino Buchholz, Model and full scale high-lift wing wind tunnel experiments dedicated to airframe noise reduction, Aerospace. Sci. Technol. 5 27–33. 2001.
Leung Choi Cho, Pierre Lempereurn, aircraft airframe noise and installation effects research studies, Air and Space Europe. vol. 1, No 3. 1999.
J. C. Hardin, Noise radiation from the side edges of flaps, American Institute of Aeronautics and Astronautics Journal 18 (5) 549–552. 1980.
S. A. McInerny, W. C. Meecham, P. T. Soderman, An experimental investigation of wing tip turbulence with applications to aero sound, AIAA Paper 86-1918. 1986.
D. G. Crighton, Airframe noise, aeroacoustics of Flight Vehicles: Theory and Practice, NASA RP-1258, Vol. 1, pp. 391–447. 1991.
Y. P. Guo, Prediction of flap edge noise, AIAA Paper 99-1804, 1999.
T. F. Brooks, W. M. Humphreys, Flap-edge aeroacoustic measurements and predictions, Journal of Sound and Vibration 261 31–74.2003.
J. C. Ross, B. L. Storms, H. Kumagai, Aircraft flyover noise reduction using lower-surface flap-tip fences, NASA CDTM-21006. 1995.
B. L. Storms, T. T. Takahashi, W. C. Horne, J. C. Ross, R. P. Dougherty, J. R. Underbrink, Flap-tip treatments for the reduction of lift-generated noise, NASA CDTM-21006. 1996.
Y. P. Guo, M. C. Joshi, Noise characteristics of aircraft high lifts systems, American Institute of Aeronautics and Astronautics Journal 41 (7) 1247–1256. 2003.
Y. P. Guo, P. Bent, K. Yamamoto, M. C. Joshi, Surface pressure fluctuations on aircraft high lift system and their correlation with far field noise, Journal of Fluid Mechanics 415 175–202. 2000.
Yueping Guo, on noise reduction by flap side edge fences, Journal of Sound and Vibration 277 369–390. 2004.
Michel, U., Barsikow, B., Helbig, J., Hellmig, M., and Schüttpelz, M., “Flyover Noise Measurements on Landing Aircraft with a Microphone Array,” AIAA Paper 98-2336, May 1998.
Piet, J.-F., Elias, G., and Lebigot, P., “Localization of Acoustic Sources from a Landing Aircraft with a Microphone Array,” AIAA Paper 99-1811, May 1999.
Michel, U. and Qiao, W., “Directivity of Landing-Gear Noise Based on Flyover Measurements,” AIAA-99-1956, May 1999.
Pott-Pollenske, M., Dobrzynski, W., Buchholz, H., Gehlhar, B., and Walle, F., “Validation of a Semiempirical Airframe Noise Prediction Method through Dedicated A319 Flyover Noise Measurements,” AIAA Paper 2002-2470, May 2002.
Stoker, R., Guo, Y., Streett, C., and Burnside, N., “Airframe Noise Source Locations of a 777 Aircraft in Flight and Comparisons with Past Model Tests,” AIAA Paper 2003-3232, May 2003.
Guo, Y, A Study on Local Flow Variations for Landing Gear Noise Research," May 5{7 2008, AIAA Paper No. 2008-2915, 14th AIAA/CEAS Aerodynamics Conference (29th AIAA Aeroacoustics Conference).
Stoker, R. W. Landing Gear Noise Test Report," NASA Contractor Informal Report NAS1-97040, Boeing, 1999.
Kipersztok, O. and Senguptat, G., Flight Test of the 747-JT9D for Airframe Noise," AIAA Journal of Aircraft, Vol. 19, No. 12, December 1982, pp. 1061.
Stoker, R. W. and Sen, R., An Experimental Investigation of Airframe Noise Using a Model-Scale Boeing 777, AIAA Paper No. A01-16784, 39th AIAA Aerospace Sciences Meeting & Exhibit" January 2001.
Lockard, D. P, Khorrami, M. R., and Li, F, High Resolution Calculation of Landing Gear noise, AIAA Paper No. 2004-2887, 10th AIAA/CEAS Aeroacoustics Conference " May 10, 13 2004.
R. J. Jeracki, “Comprehensive Report on Fan Performance From Duct Rake Instrumentation on 1.294 Pressure Ratio, 806 ft/sec Tip Speed Turbofan Simulator Models,” NASA TM-2006-213863 (2006).
C. Polacsek, Reduction of fan rotor–stator interacting modes using a novel design: an experimental study, Proceedings of the Sixth International Congress on Sound and Vibration (ISCV), Copenhagen, 1999.
R. E. Kraft, K. B. Kontos, Theoretical implications of active noise control for turbofan engines, 15th aero acoustics Conference, Long Beach, CA, October 1993.
R. H. Thomas, R. A. Burdisso, R. A. Fuller, C. R. O’Brien, Active control of fan noise from a turbofan engine, American Institute of Aeronautics and Astronautics Journal 32 (1) 23–30. 1994.
T. Ishii, H. Kobayashi, H. Oinuma, Wave-form technique for reduction of tones radiated from a ducted fan, AIAA No. 97-1664-CP,, pp. 619–625. 1997.
S. Sawyer, S. Fleeter, Active control of discrete-frequency noise generated by rotor–stator interactions, AIAA No. 97-1663-CP, pp. 609–617. 1997.
D. L. Sutliff, Z. Hu, F. G. Pla, L. J. Heidelberg, Active noise control of low speed fan rotor–stator modes, Third AIAA/CEAS Aero acoustic Conference, Atlanta, GA, 1997.
W. Just, I. U. Borchers, H. Antoine, E. Bouty, J. Zillmann, R. Maier, Control of fan noise by active stators, Seventh AIAA/CEAS, Maastricht. 2001.
A. R. D. Curtis, Active Control of Fan Noise by Vane Actuators, BBN Technologies, Cambridge, MA, NASA/CR- 1999-209156. 1999.
Dennis L. Huff, Noise Reduction Technologies for Turbofan Engines, 35th International Congress and Exposition on Noise Control Engineering (INTER–NOISE 2006) sponsored by the International Institute of Noise Control Engineering Honolulu, HI, December 3–6. 2006.
H. F. Olson, E. G. May, Electronic sound absorber, Journal of the Acoustical Society of America 25 1130–1136. 1953.
D. Guicking, E. Lorenz, An active sound absorber with porous plate, Journal of Vibration and Acoustics 106 389–392. 1984.
F. P. Mechel, Hybrider Schallda mplfer, Patent No DE4027511.
D. Thenail, Control active impedance optimization des performances, PhD Thesis, Ecole Centrale de Lyon, Ecully, France, 1995.
M. Furstoss, D. Thenail, M. A. Galland, Surface impedance control for sound absorption: direct and hybrid passive/active strategies, Journal of Sound and Vibration 203 (2) 219–236. 1997.
S. Beyene, A. Burdisso, A new passive/active noise absorption system, Journal of the Acoustical Society of America 101 (3) 1512–1515. 1997.
P. Cobo, J. Pfretzschner, M. Cuesta, D. K. Anthony, Hybrid passive–active absorption using microperforated panels, Journal of the Acoustical Society of America 116 (4) 2118–2125. 2004.
Suddaby, P. A study of the velocity fluctuations in the noise producing region of jet. MSCThesis, Cranfield University, 1964.
Lighthill, M. J. On sound generated aerodynamically. I. General theory. In Proceedings of the Royal Society of London, Series A211, pp. 564–587. 1952.
Lighthill, M. J. On sound generated aerodynamically. II. Turbulence as a source of sound. In Proceedings of the Royal Society of London, Series A222, pp. 1–32.1952.
H. H. Hubbard, Aeroacoustic of fligh veheles: Theory and practice, volume 1: noise sources, Nasa Langly Research center 1992.
Brian C. Kuo, Nesrin Sarigul-Klijn, Conceptual study of micro-tab device in airframe noise reduction (I) 2D computation, Aerospace Science and Technology 14 307–315.2010.
Mathias Steger, Ulf Michel, Graham Ashcroft, and Frank Thiele, Turbofan Tone Noise Reduction by Flow-Induced Unsteady Blade Forces, Active Flow Control II, NNFM 108, pp. 157–170. 2010.
Schulz, J, Neise, W., Moser, M.: Active control of the blade passage frequency noise level of an axial fan with aero acoustic sound sources. Noise Control Engineering Journal 54, 33–40 2006.
Ashcroft, G., Schulz, J. Numerical modeling of wake-jet interaction with application to active noise control in turbo machinery. AIAA Paper 2004-2853 2004.
Fathollah Ommi and Mohammadreza Azimi, main fan noise mitigation technologies in turbofan engines, Taylor and francis, ISSN 1648-7788 / eISSN 1822-4180, Volume 18 (3): 141-146. 2014.
Khaletskiy, Y. D, Effectiveness of Combined Aircraft Engine Noise uppresions. Acoustical Physics, vol. 58, № 4, pp. 510-515. 2012.
Osipov, А. А., Reent, K. S., Mathematical modelling of sound propagation in flow duct with impedance walls. Acoustical Physics, vol. 58, № 4, pp. 467-480. 2012.
Envia, E., Fan noise reduction: an overview. International J. of Aero acoustics. vol. 1, no 1, pp. 43-64. 2002.
Rao, G. V. R., Use of Leaning Vanes for Fan Noise Reduction. 10th Aerospace Sciences Meeting. San Diego, USA. AIAA paper. no. 72-126, pp. 1-16. 1972.
Envia, E., Nallasamy, M., Design selection and analysis of a swept and leaned stator concept. Journal of Sound and Vibration. vol. 228, no 4, pp. 793-836. 1999.
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