Bücher zum Thema „Aircraft cabins Noise Measurement“
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Cole, J. E. Structureborne noise measurements on a small twin-engine aircraft. Hampton, Va: Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenHeller, H. Aircraft exterior noise measurement and analysis techniques. Neuilly sur Seine: Agard, 1991.
Den vollen Inhalt der Quelle findenHeller, H. Aircraft exterior noise measurement and analysis techniques. Neuilly-sur-Seine: AGARD, 1991.
Den vollen Inhalt der Quelle findenMcCurdy, David A. Annoyance caused by aircraft en route noise. Hampton, Va: Langley Research Center, 1992.
Den vollen Inhalt der Quelle findenSimpson, K. C. Vancouver International Airport aircraft noise monitoring system selection of remote monitoring sites. Vancouver, B.C: Transport Canada, 1985.
Den vollen Inhalt der Quelle findenSoderman, 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.
Den vollen Inhalt der Quelle findenSoderman, 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.
Den vollen Inhalt der Quelle findenSoderman, 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.
Den vollen Inhalt der Quelle findenBrase, 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.
Den vollen Inhalt der Quelle findenBlock, P. J. W. Directory and trends of noise generated by a propeller in a wake. Hampton, Va: Langley Research Center, 1986.
Den vollen Inhalt der Quelle findenTubbs, Randy L. Horizon Air, Seattle, Washington. [Atlanta, Ga.]: Dept. of Health and Human Services, Centers for Disease Control and Prevention, National Institute for Occupational Safety and Health, 2004.
Den vollen Inhalt der Quelle findenTubbs, Randy L. Horizon Air, Seattle, Washington. [Atlanta, Ga.]: Dept. of Health and Human Services, Centers for Disease Control and Prevention, National Institute for Occupational Safety and Health, 2004.
Den vollen Inhalt der Quelle findenTubbs, Randy L. Horizon Air, Seattle, Washington. [Atlanta, Ga.]: Dept. of Health and Human Services, Centers for Disease Control and Prevention, National Institute for Occupational Safety and Health, 2004.
Den vollen Inhalt der Quelle findenKraft, R. E. Acoustic treatment design scaling methods. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Den vollen Inhalt der Quelle findenKraft, R. E. Acoustic treatment design scaling methods. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Den vollen Inhalt der Quelle findenF, Martini K., und United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Structureborne noise measurements on a small twin-engine aircraft. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Den vollen Inhalt der Quelle findenG, Rackl Robert, Andrianov Eduard V und Langley Research Center, Hrsg. Flight test measurements from the Tu-144LL structure/cabin noise experiment. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.
Den vollen Inhalt der Quelle findenAliabadi, M. H., und Ignazio Dimino. Active Control of Aircraft Cabin Noise. Imperial College Press, 2015.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Asymptotic modal analysis of a rectangular acoustic cavity. [Washington, DC: National Aeronautics and Space Administration, 1988.
Den vollen Inhalt der Quelle findenB, Bliss Donald, und United States. National Aeronautics and Space Administration., Hrsg. Aircraft interior noise reduction by alternate resonance tuning: Progress report for the period ending December, 1990 : final progress report. Durham, NC: Dept. of Mechanical Engineering and Materials Science, Duke University, 1990.
Den vollen Inhalt der Quelle findenInteraction of airborne and structureborne noise radiated by plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Interaction of airborne and structureborne noise radiated by plates. [Washington, DC]: National Aeronautics and Space Administration, 1986.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Interaction of airborne and structureborne noise radiated by plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Interaction of airborne and structureborne noise radiated by plates. [Washington, DC]: National Aeronautics and Space Administration, 1986.
Den vollen Inhalt der Quelle findenR, Fuller C., und United States. National Aeronautics and Space Administration., Hrsg. An improved source model for aircraft interior noise studies. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Den vollen Inhalt der Quelle findenLaboratory test and acoustic analysis of cabin treatment for propfan test assessment aircraft. Burbank, Calif: Lockheed Aeronautical Systems Company, 1991.
Den vollen Inhalt der Quelle finden1870-1952, Tillema H. F., MacGregor G. R und Langley Research Center, Hrsg. Application of analysis techniques for low frequency interior noise and vibration of commercial aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Den vollen Inhalt der Quelle findenNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., Hrsg. Aircraft exterior noise measurement and analysis techniques. Neuilly sur Seine, France: AGARD, 1991.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Signal processing of aircraft flyover noise. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Den vollen Inhalt der Quelle findenA, Clevenson Sherman, Stephens David G und Langley Research Center, Hrsg. The development of interior noise and vibration criteria. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Den vollen Inhalt der Quelle finden1870-1952, Tillema H. F., Marshall Steven E, Langley Research Center und Boeing Commercial Airplane Company, Hrsg. Evaluation of analysis techniques for low frequency interior noise and vibration of commercial aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Combustion noise from gas turbine aircraft engines measurement of far-field levels. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.
Den vollen Inhalt der Quelle findenU.S. Department of Transportation. Aircraft Source Noise Measurement Studies: Summary of Measurements, Data and Analysis. CreateSpace Independent Publishing Platform, 2013.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division. und United States. Army Aviation Systems Command., Hrsg. Measurement resolution of noise directivity patterns from acoustic flight tests. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Den vollen Inhalt der Quelle findenT, Ohler Eric, und Construction Engineering Research Laboratories (U.S.), Hrsg. Software development plan for the Assessment System for Aircraft Noise, version 2.0. [Champaign, Ill.]: US Army Corps of Engineers, Construction Engineering Research Laboratories, 1996.
Den vollen Inhalt der Quelle findenM, Golebiowski, Seiner John M und United States. National Aeronautics and Space Administration., Hrsg. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.
Den vollen Inhalt der Quelle findenM, Golebiowski, Seiner John M und United States. National Aeronautics and Space Administration., Hrsg. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.
Den vollen Inhalt der Quelle findenM, Golebiowski, Seiner John M und United States. National Aeronautics and Space Administration., Hrsg. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Comparison of advanced turboprop and conventional jet and propeller aircraft flyover noise annoyance: Preliminary results. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.
Den vollen Inhalt der Quelle finden1961-, Schein David B., Gridley Doreen, Langley Research Center und United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Hrsg. Analytical study of acoustic response of a semireverberant enclosure with application to active noise control. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Den vollen Inhalt der Quelle findenGround-recorded sonic boom signatures of F-18 aircraft in formation flight. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1995.
Den vollen Inhalt der Quelle findenA, Haering Edward, und Hugh A. Dryden Flight Research Center., Hrsg. Ground-recorded sonic boom signatures of F-18 aircraft in formation flight. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1995.
Den vollen Inhalt der Quelle findenA, Haering Edward, und Hugh A. Dryden Flight Research Center., Hrsg. Ground-recorded sonic boom signatures of F-18 aircraft in formation flight. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1995.
Den vollen Inhalt der Quelle findenThe accuracy of parameter estimation in system identification of noisy aircraft load measurement. [Los Angeles, Calif.]: University of California, Los Angeles, 1994.
Den vollen Inhalt der Quelle findenH, Saiyed Naseem, und United States. National Aeronautics and Space Administration., Hrsg. Characteristics of residual mixing noise from internal fan/core mixers. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Den vollen Inhalt der Quelle findenF, Peretti Linda, und United States. National Aeronautics and Space Administration., Hrsg. Asymptotic modal analysis and statistical energy analysis. [Washington, DC: National Aeronautics and Space Administration, 1990.
Den vollen Inhalt der Quelle findenE, Kraft R., und Langley Research Center, Hrsg. Acoustic treatment design scaling methods: Phase II final report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2003.
Den vollen Inhalt der Quelle findenE, Kraft R., und Langley Research Center, Hrsg. Acoustic treatment design scaling methods: Phase II final report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2003.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Experimental measurement of structural power flow on an aircraft fuselage: Progress report, grant number NAG-1-685. Boca Rotan, Fla: Florida Atlantic University, College of Engineering, Dept. of Ocean Engineering, Center for Acoustics and Vibrations, 1989.
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