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1

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

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2

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

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3

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

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4

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

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5

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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6

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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7

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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8

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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10

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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11

Tubbs, 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.

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12

Tubbs, 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.

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13

Tubbs, 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.

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14

Kraft, R. E. Acoustic treatment design scaling methods. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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15

Kraft, R. E. Acoustic treatment design scaling methods. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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16

F, Martini K., e United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Structureborne noise measurements on a small twin-engine aircraft. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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17

G, Rackl Robert, Andrianov Eduard V e Langley Research Center, eds. Flight test measurements from the Tu-144LL structure/cabin noise experiment. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

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18

Aliabadi, M. H., e Ignazio Dimino. Active Control of Aircraft Cabin Noise. Imperial College Press, 2015.

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19

United States. National Aeronautics and Space Administration., ed. Asymptotic modal analysis of a rectangular acoustic cavity. [Washington, DC: National Aeronautics and Space Administration, 1988.

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20

B, Bliss Donald, e United States. National Aeronautics and Space Administration., eds. 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.

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21

Interaction of airborne and structureborne noise radiated by plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

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22

United States. National Aeronautics and Space Administration., ed. Interaction of airborne and structureborne noise radiated by plates. [Washington, DC]: National Aeronautics and Space Administration, 1986.

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23

Center, Langley Research, ed. Interaction of airborne and structureborne noise radiated by plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

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24

United States. National Aeronautics and Space Administration., ed. Interaction of airborne and structureborne noise radiated by plates. [Washington, DC]: National Aeronautics and Space Administration, 1986.

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25

R, Fuller C., e United States. National Aeronautics and Space Administration., eds. An improved source model for aircraft interior noise studies. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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26

Laboratory test and acoustic analysis of cabin treatment for propfan test assessment aircraft. Burbank, Calif: Lockheed Aeronautical Systems Company, 1991.

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27

1870-1952, Tillema H. F., MacGregor G. R e Langley Research Center, eds. 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.

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28

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., ed. Aircraft exterior noise measurement and analysis techniques. Neuilly sur Seine, France: AGARD, 1991.

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29

Center, Langley Research, ed. Signal processing of aircraft flyover noise. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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30

A, Clevenson Sherman, Stephens David G e Langley Research Center, eds. The development of interior noise and vibration criteria. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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31

1870-1952, Tillema H. F., Marshall Steven E, Langley Research Center e Boeing Commercial Airplane Company, eds. 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.

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32

United States. National Aeronautics and Space Administration., ed. Combustion noise from gas turbine aircraft engines measurement of far-field levels. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.

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33

U.S. Department of Transportation. Aircraft Source Noise Measurement Studies: Summary of Measurements, Data and Analysis. CreateSpace Independent Publishing Platform, 2013.

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34

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. e United States. Army Aviation Systems Command., eds. 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.

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35

T, Ohler Eric, e Construction Engineering Research Laboratories (U.S.), eds. 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.

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36

M, Golebiowski, Seiner John M e United States. National Aeronautics and Space Administration., eds. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.

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37

M, Golebiowski, Seiner John M e United States. National Aeronautics and Space Administration., eds. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.

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38

M, Golebiowski, Seiner John M e United States. National Aeronautics and Space Administration., eds. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.

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39

Center, Langley Research, ed. 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.

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40

1961-, Schein David B., Gridley Doreen, Langley Research Center e United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. 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.

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41

Ground-recorded sonic boom signatures of F-18 aircraft in formation flight. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1995.

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42

A, Haering Edward, e Hugh A. Dryden Flight Research Center., eds. Ground-recorded sonic boom signatures of F-18 aircraft in formation flight. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1995.

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43

A, Haering Edward, e Hugh A. Dryden Flight Research Center., eds. Ground-recorded sonic boom signatures of F-18 aircraft in formation flight. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1995.

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44

The accuracy of parameter estimation in system identification of noisy aircraft load measurement. [Los Angeles, Calif.]: University of California, Los Angeles, 1994.

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45

H, Saiyed Naseem, e United States. National Aeronautics and Space Administration., eds. Characteristics of residual mixing noise from internal fan/core mixers. [Washington, DC]: National Aeronautics and Space Administration, 1997.

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46

F, Peretti Linda, e United States. National Aeronautics and Space Administration., eds. Asymptotic modal analysis and statistical energy analysis. [Washington, DC: National Aeronautics and Space Administration, 1990.

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47

E, Kraft R., e Langley Research Center, eds. Acoustic treatment design scaling methods: Phase II final report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2003.

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48

E, Kraft R., e Langley Research Center, eds. Acoustic treatment design scaling methods: Phase II final report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2003.

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49

Center, Langley Research, ed. 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.

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50

United States. National Aeronautics and Space Administration., ed. 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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