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Thematische Bibliographien / Aircraft cabins Noise Measurement

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Zeitschriftenartikel
Dissertationen
Bücher
Buchteile
Konferenzberichte
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Auswahl der wissenschaftlichen Literatur zum Thema „Aircraft cabins Noise Measurement“

Autor: Grafiati

Veröffentlicht am 4. Juni 2021

Zuletzt aktualisiert am 1. Februar 2022

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Zeitschriftenartikel zum Thema "Aircraft cabins Noise Measurement"

1

Hughes, Stanley T., and Jefferson Koonce. "Cabin Noise Levels in Single Engine General Aviation Aircraft." Proceedings of the Human Factors Society Annual Meeting 30, no. 14 (September 1986): 1381–85. http://dx.doi.org/10.1177/154193128603001408.

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Sound level measurements were made on several of the most popular general aviation aircraft produced. Measurements were taken at various flight milestones such as; run up, taxi, climb, cruise power and descent. For each of the aircraft a time weighted mission sound level was obtained, using three different mission scenarios, varying only in flight time. For each of the three scenarios, and for all aircraft, the time weighted noise values obtained were an or exceeded the 85 dBA limit recommended by NIOSH. The results of this study indicate that a substantial percentage of general aviation pilot

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Kong, Qing Fu, Yu Liang Dai, Shi Jian Zhu, and Jia Ming Wu. "Experimental Study on an Active Noise Control System for Turboprop Driven Aircraft." Applied Mechanics and Materials 333-335 (July 2013): 2142–45. http://dx.doi.org/10.4028/www.scientific.net/amm.333-335.2142.

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In order to find a solution to the control of low frequency noise in the cabin of turboprop driven aircraft, an experimental active noise control (ANC) system is introduced in the paper, which consists of vibroacoustic field analogue subsystem, acoustic field measurement subsystem and acoustic barrier exciter subsystem. Effects of both different spaces between the primary sound source and secondary sound source of the ANC system and different frequency noises on noise-reduction result are investigated based on the experimental platform. Results of the experiment show a significant potential of

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Joshi, Pankaj, Frank Khelfa, Hendrik Lehmkuhl, Patrick Cordes, Patrick Naujoks, Thorsten Scharowsky, and Kay Kochan. "Design, development and testing of digital MEMS pressure sensor array for full-scale vibroacoustic measurements." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 263, no. 2 (August 1, 2021): 4343–54. http://dx.doi.org/10.3397/in-2021-2671.

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This manuscript addresses design, development, and application of micro-electro-mechanical systems (MEMS) based digital pressure sensor array for vibroacoustic measurements. These vibroacoustic measurements were conducted on a A320 type single aisle aircraft demonstrator subjected to broadband as well as tonal excitations. Cabin noise levels were measured with both condenser microphones as well as digital MEMS pressure sensor array. The measured cabin noise shows strong qualitative as well as quantitative agreement between both type of measurement devises for full scale cabin noise measurement

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Spehr, Carsten, Daniel Ernst, and Hans-Georg Raumer. "MEMS microphone intensity array for cabin noise measurements." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 263, no. 3 (August 1, 2021): 3023–34. http://dx.doi.org/10.3397/in-2021-2288.

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Aircraft cabin noise measurements in flight are used toto quantify the noise level, and to identify the entry point of acoustic energy into the cabin. Sound intensity probes are the state-of-the-art measurement technique for this task. During measurements, additional sound absorbing material is used to ease the rather harsh acoustic measurement environment inside the cabin. In order to decrease the expensive in-flight measurement time, an intensity array approach was chosen. This intensity probe consists of 512 MEMS-Microphones. Depending on the frequency, these microphones can be combined as

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PAČAIOVÁ, Hana, Marianna TOMAŠKOVÁ, Michaela BALÁŽIKOVÁ, and Jozef KRAJŇÁK. "Analysis of air-traffic threats." Scientific Journal of Silesian University of Technology. Series Transport 110 (March 1, 2021): 143–55. http://dx.doi.org/10.20858/sjsutst.2021.110.12.

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Globally, air transport has seen a greater increase in recent years. This manuscript is divided into three parts for analysing the negative effects of aviation. The first part is focused on the identification of sources of aircraft noise. While the second part of this article describes the basic principles of the construction and operation of an aircraft jet engine concerning the gaseous emissions produced by such an engine (Third part missing?). The main benefit of this article is the evaluation of the reliability of the human factor because the human factor is an integral part of technical s

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Schüür, Jens, Lukas Oppermann, Achim Enders, Rafael R. Nunes, and Carl-Henrik Oertel. "Emission analysis of large number of various passenger electronic devices in aircraft." Advances in Radio Science 14 (September 28, 2016): 129–37. http://dx.doi.org/10.5194/ars-14-129-2016.

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Abstract. The ever increasing use of PEDs (passenger or portable electronic devices) has put pressure on the aircraft industry as well as operators and administrations to reevaluate established restrictions in PED-use on airplanes in the last years. Any electronic device could cause electromagnetic interference to the electronics of the airplane, especially interference at receiving antennas of sensitive wireless navigation and communication (NAV/COM) systems. This paper presents a measurement campaign in an Airbus A320. 69 test passengers were asked to actively use a combination of about 150

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Zettel, Sebastian, René Winter, Marco Norambuena, Marc Böswald, Martin Richter, and Gregor Tanner. "Finite element method and dynamical energy analysis in vibro-acoustics - A comparative study." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 263, no. 5 (August 1, 2021): 1712–22. http://dx.doi.org/10.3397/in-2021-1906.

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Future aircraft concepts utilizing innovative lightweight structures and novel propulsion concepts are a necessity for long term sustainable air travel. These concepts pose new challenges for the vibro-acoustic assessment of cabin structures and the associated noise impact on passengers. Finite Element (FE) models derived from aircraft pre-design data are not optimized for use in acoustic analyses, i.e. the mesh is too coarse to provide meaningful results while setting up Statistical Energy Analysis models for this specific purpose is adding another time-consuming step. A possible alternative,

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Ross, Colin F. "Active noise control in aircraft cabins." Journal of the Acoustical Society of America 105, no. 2 (February 1999): 1243. http://dx.doi.org/10.1121/1.425969.

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Kloss, Corinna, Vicheith Tan, J. Brian Leen, Garrett L. Madsen, Aaron Gardner, Xu Du, Thomas Kulessa, et al. "Airborne Mid-Infrared Cavity enhanced Absorption spectrometer (AMICA)." Atmospheric Measurement Techniques 14, no. 8 (August 2, 2021): 5271–97. http://dx.doi.org/10.5194/amt-14-5271-2021.

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Abstract. We describe the Airborne Mid-Infrared Cavity enhanced Absorption spectrometer (AMICA) designed to measure trace gases in situ on research aircraft using Off-Axis Integrated Cavity Output Spectroscopy (OA-ICOS). AMICA contains two largely independent and exchangeable OA-ICOS arrangements, allowing for the simultaneous measurement of multiple substances in different infrared wavelength windows tailored to scientific questions related to a particular flight mission. Three OA-ICOS setups have been implemented with the aim to measure OCS, CO2, CO, and H2O at 2050 cm−1; O3, NH3, and CO2 at

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Takahashi, Kosaku, Hirotaka Monzen, Toshihiro Yamaoka, Koji Kusumoto, Kazuhiro Bansaku, Jyunichi Kimoto, Akira Isoe, Yasuo Hirose, Tomio Sanda, and Yuji Matsuzaki. "Noise and vibration reduction technology in aircraft cabins." Advanced Composite Materials 13, no. 1 (January 2004): 67–80. http://dx.doi.org/10.1163/1568551041408787.

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Dissertationen zum Thema "Aircraft cabins Noise Measurement"

1

Kestell, Colin D. "Active control of sound in a small single engine aircraft cabin with virtual error sensors." Title page, abstract and contents only, 2000. http://web4.library.adelaide.edu.au/theses/09PH/09phk423.pdf.

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Robert, Rene Jean. "Measuring noise level reduction using an artificial noise source." Thesis, Georgia Institute of Technology, 2015. http://hdl.handle.net/1853/54480.

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Buildings located near airports may be subjected to significant noise levels due to aircraft flyovers. Aircraft noise is particularly annoying when compared to other traffic noises due to its intermittent nature. While noise control is typically performed at the source, sound insulation programs are in place to improve the acoustic performance of a residence affected by the flyovers. Noise Level Reduction (NLR) is a common metric used in the United States to determine whether a residence qualifies for such programs. Sound insulation programs are available to houses that have an indoor Day Nigh

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Camponogara, Ândrei. "Measurement and characterization of aircraft PLC channels." Universidade Federal de Juiz de Fora (UFJF), 2016. https://repositorio.ufjf.br/jspui/handle/ufjf/5516.

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Submitted by Renata Lopes (renatasil82@gmail.com) on 2017-07-21T13:33:19Z No. of bitstreams: 1 andreicamponogara.pdf: 136426958 bytes, checksum: 46cc006b7976ec02d48cf7b3ce754288 (MD5)<br>Approved for entry into archive by Adriana Oliveira (adriana.oliveira@ufjf.edu.br) on 2017-08-09T13:17:24Z (GMT) No. of bitstreams: 1 andreicamponogara.pdf: 136426958 bytes, checksum: 46cc006b7976ec02d48cf7b3ce754288 (MD5)<br>Made available in DSpace on 2017-08-09T13:17:24Z (GMT). No. of bitstreams: 1 andreicamponogara.pdf: 136426958 bytes, checksum: 46cc006b7976ec02d48cf7b3ce754288 (MD5) Previous issue

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Thomas, Ashwin Paul. "Simulated and laboratory models of aircraft sound transmission." Thesis, Georgia Institute of Technology, 2014. http://hdl.handle.net/1853/52319.

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With increased exposure to transportation noise, there have been continued efforts to help insulate homes from aircraft noise. Current aircraft noise guidelines are based primarily on outdoor sound levels. As people spend the majority of their time indoors, however, human perception is evidently more related to indoor sound levels. Investigations are being made to provide further insight into how typical residential constructions affect indoor response. A pilot study has built a single-room "test house", according to typical construction for mixed-humid climate regions, and has directly measur

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Issarayangyun, Tharit Civil &amp Environmental Engineering Faculty of Engineering UNSW. "Aircraft noise and public health : acoustical measurement and social survey around Sydney (Kingsford Smith) Airport." Awarded by:University of New South Wales. Civil and Environmental Engineering, 2005. http://handle.unsw.edu.au/1959.4/22394.

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The development of major commercial airports promotes the air transport industry and generates positive economic benefits to the airport and to its host economy. However, external costs are associated with these benefits. Any increase in aircraft movement causes negative environmental impacts, especially noise pollution. Governments have reduced aircraft noise levels at their sources, or introduced aircraft noise management strategies (ANMS); however the problems have never been satisfactorily resolved. This research aims at developing a better understanding of the impacts of aircraft noise on

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Thabet, Rihab El Houda. "Détection de défauts des systèmes non linéaires à incertitudes bornées continus." Thesis, Bordeaux, 2014. http://www.theses.fr/2014BORD0283/document.

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La surveillance des systèmes industriels et/ou embarqués constitue une préoccupation majeure en raison de l’accroissement de leur complexité et des exigences sur le respect des profilsde mission. La détection d’anomalies tient une place centrale dans ce contexte. Fondamentalement,les procédures de détection à base de modèles consistent à comparer le fonctionnement réel dusystème avec un fonctionnement de référence établi à l’aide d’un modèle sans défaut. Cependant,les systèmes à surveiller présentent souvent des dynamiques non linéaires et difficiles à caractériserde manière exacte. L’approche

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Kestell, Colin D. (Colin David). "Active control of sound in a small single engine aircraft cabin with virtual error sensors." 2000. http://thesis.library.adelaide.edu.au/public/adt-SUA20010216.164243/index.html.

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Bibliography: p. 199-207. Electronic publication; full text available in PDF format; abstract in HTML format. Describes the basis of a theoretical and experimental project, directed at the design and evaluation of a practical active noise control system suitable for a single light engine aircraft. The performance of virtual sensors were evaluated both analytically and experimentally in progressively more complex environments to identify their capabilities and limitations. Electronic reproduction.[Australia] :Australian Digital Theses Program,2001.

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Lee, Tsuan-Hsi, and 李纘錫. "Noise Measurement and Analysis of ship cabins." Thesis, 2016. http://ndltd.ncl.edu.tw/handle/50828305491709483889.

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碩士<br>國立高雄海洋科技大學<br>輪機工程研究所<br>104<br>Since the living standard of human race is improving, the ship owner has more and more strict requirements on vibration and noise problem of the ship. Firstly, this thesis will carry out the measurement and analysis of the ship noise. Then, the noise source will be identified. Finally, recommendations for noise improvement of ship will be given. Keywords: ship, noise, noise control

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Rocha, Joana Luiz Torres da. "Coupled structural-acoustic analytical models for the prediction of turbulent boundary-layer-induced noise in aircraft cabins." Thesis, 2010. http://hdl.handle.net/1828/6834.

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Significant interior noise and vibrations in aircraft cabins are generated by the turbulent flow over the fuselage. The turbulent boundary layer (TBL) excitation is the most important noise source for jet powered aircraft during cruise flight. Reduced levels of interior noise are desirable both for comfort and health reasons. However, to efficiently design noise control systems, and to design new and optimized structures that are more efficient in the noise reduction, a clearer understanding of the sound radiation and transmission mechanisms is crucial. This task is far from being strai

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Issarayangyun, Tharit. "Aircraft noise and public health : acoustical measurement and social survey around Sydney, Kingsford Smith Airport /." 2005. http://www.library.unsw.edu.au/~thesis/adt-NUN/public/adt-NUN20050830.232517/index.html.

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Bücher zum Thema "Aircraft cabins Noise Measurement"

1

Cole, J. E. Structureborne noise measurements on a small twin-engine aircraft. Hampton, Va: Langley Research Center, 1988.

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Heller, H. Aircraft exterior noise measurement and analysis techniques. Neuilly sur Seine: Agard, 1991.

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Heller, H. Aircraft exterior noise measurement and analysis techniques. Neuilly-sur-Seine: AGARD, 1991.

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McCurdy, David A. Annoyance caused by aircraft en route noise. Hampton, Va: Langley Research Center, 1992.

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Simpson, K. C. Vancouver International Airport aircraft noise monitoring system selection of remote monitoring sites. Vancouver, B.C: Transport Canada, 1985.

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Soderman, Paul T. J-85 jet engine noise measured in the ONERA S1 Wind Tunnel and extrapolated to far field. Moffett Field, Calif: Ames Research Center, 1991.

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Soderman, Paul T. J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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Soderman, Paul T. J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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9

Brase, L. O. Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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Block, P. J. W. Directory and trends of noise generated by a propeller in a wake. Hampton, Va: Langley Research Center, 1986.

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Buchteile zum Thema "Aircraft cabins Noise Measurement"

1

Fidell, Sanford, and Vincent Mestre. "Aircraft Noise Measurement and Modeling." In A Guide To U.S. Aircraft Noise Regulatory Policy, 59–74. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-39908-5_4.

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2

Taylor, J. O. "The Use of Barkhausen Noise for the Measurement of Residual Stresses in Aircraft Parts." In Review of Progress in Quantitative Nondestructive Evaluation, 1715–22. Boston, MA: Springer US, 1997. http://dx.doi.org/10.1007/978-1-4615-5947-4_224.

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3

Rodríguez Timaná, Luis Carlos, Diego Fernando Saavedra Lozano, María Fernanda Díaz Velásquez, and Javier Ferney Castillo García. "Technical Feasibility for the Mobile Measurement of Noise Pollution by Remotely Piloted Aircraft System." In Communications in Computer and Information Science, 219–30. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-42531-9_18.

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Konferenzberichte zum Thema "Aircraft cabins Noise Measurement"

1

Greßkowski, Julian, Sten Böhme, and Delf Sachau. "Global Active Noise Control in Aircraft Cabins." In 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-3242.

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2

da Rocha, Joana, Afzal Suleman, and Fernando Lau. "Prediction of Turbulent Flow-Induced Noise in Aircraft Cabins." In ASME 2010 International Mechanical Engineering Congress and Exposition. ASMEDC, 2010. http://dx.doi.org/10.1115/imece2010-39231.

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Flow-induced noise in aircraft cabins can be predicted through analytical models or numerical methods. However, the analytical methods existent nowadays were obtained for simple structures and cabins, in which, usually, a single panel is excited by the turbulent flow, and coupled with an acoustic enclosure. This paper discusses the development of analytical models for the prediction of aircraft cabin noise induced by the external turbulent boundary layer (TBL). The coupled structural-acoustic analytical model is developed using the contribution of both structural and acoustic natural modes. Wh

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Bonillo, Alejandro. "Optimization of structural countermeasures for noise attenuation in aircraft cabins." In 19th AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-2230.

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Dolmans, Jeroen, and Howard Patrick. "The application of active noise control in single engine general aviation aircraft cabins." In 4th AIAA/CEAS Aeroacoustics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-2235.

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Grewal, A., D. Zimcik, L. Hurtubise, B. Leigh, A. Grewal, D. Zimcik, L. Hurtubise, and B. Leigh. "Active noise and vibration control of turboprop aircraft cabins using multiple piezoelectric actuators." In 3rd AIAA/CEAS Aeroacoustics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-1638.

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Turgut, Enis, Mustafa Cavcar, Ozan D. Yay, Elif Yilmaz, Mehmet Ucarsu, Oznur Usanmaz, Tuncay Dogeroglu, Kadir Armutlu, and Richard Miake-Lye. "Test Cell Emission Measurement of Commercial Aircraft Engine: CFM56-7B26." In AIAA/3AF Aircraft Noise and Emissions Reduction Symposium. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2014. http://dx.doi.org/10.2514/6.2014-3167.

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Lee, Sang Soo. "Phased-Array Measurement of Modern Regional Aircraft Turbofan Engine Noise." In 12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-2653.

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Ananthanarayanan, S., A. Magleby, and C. Furse. "Measurement and modeling of noise and interference in aircraft system." In 2010 IEEE International Symposium Antennas and Propagation and CNC-USNC/URSI Radio Science Meeting. IEEE, 2010. http://dx.doi.org/10.1109/aps.2010.5561054.

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SMITH, M. "Aircraft noise measurement - Alternatives to the standard 1-2 metresmicrophone height." In 10th Aeroacoustics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-1960.

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Chappuis, Johanna, Besluau François, and Polin Matthieu. "Air conditioning system noise measurement and characterization for aircraft ground operations." In 17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-2934.

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Berichte der Organisationen zum Thema "Aircraft cabins Noise Measurement"

1

Fidell, Sanford, Richard Howe, Barbara Tabachnick, Karl Pearsons, Laura Silvati, Matthew Sneddon, and Elizabeth Fletcher. Field Studies of Habituation to Change in Nighttime Aircraft Noise and of Sleep Motility Measurement Methods. Fort Belvoir, VA: Defense Technical Information Center, March 1998. http://dx.doi.org/10.21236/ada388876.

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