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1

Center, Langley Research, ed. An assessment of propeller aircraft noise reduction technology. National Aeronautics and Space Administration, Langley Research Center, 1995.

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2

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Aircraft propeller induced structure-borne noise. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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3

Soderman, Paul T. Acoustic and aerodynamic study of a pusher-propeller aircraft model. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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4

A, Krejsa E., and Langley Research Center, eds. Predicted and measured boundary layer refraction for advanced turboprop propeller noise. National Aeronautics and Space Administration, Langley Research Center, 1990.

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5

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Noise propagation from a four-engine, propeller-driven airplane. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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6

B, Gordon Eliott, Jeracki Robert J, and United States. National Aeronautics and Space Administration., eds. The effect of front-to-rear propeller spacing on the interaction noise at cruise conditions of a model counterrotation propeller having a reduced diameter aft propeller. National Aeronautics and Space Administration, 1988.

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7

B, Gordon Eliott, Jeracki Robert J, and United States. National Aeronautics and Space Administration., eds. The effect of front-to-rear propeller spacing on the interaction noise at cruise conditions of a model counterrotation propeller having a reduced diameter aft propeller. National Aeronautics and Space Administration, 1988.

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8

P, Woodward Richard, and United States. National Aeronautics and Space Administration., eds. Noise levels from a model turbofan engine with simulated noise control measures applied. National Aeronautics and Space Administration, 1993.

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9

Nguyen, L. Cathy. A users guide for the NASA ANOPP propeller analysis system. NASA Langley Research Center, 1997.

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10

H, Mayes William, Daniels Edward F, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Effects of propeller rotation direction on airplane interior noise levels. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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11

L, Gentry Carl, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Directivity and trends of noise generated by a propeller in a wake. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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12

United States. National Aeronautics and Space Administration., ed. Prediction of the noise from a propeller at angle of attack. National Aeronautics and Space Administration, 1990.

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13

United States. National Aeronautics and Space Administration., ed. The effect of front-to-rear propeller spacing on the interaction noise of a model counterrotation propeller at cruise conditions. National Aeronautics and Space Administration, 1987.

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14

United States. National Aeronautics and Space Administration., ed. The effect of front-to-rear propeller spacing on the interaction noise of a model counterrotation propeller at cruise conditions. National Aeronautics and Space Administration, 1987.

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15

J, Loeffler Irvin, and United States. National Aeronautics and Space Administration., eds. Inflight source noise of an advanced full-scale single-rotation propeller. National Aeronautics and Space Administration, 1991.

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16

J, Kelly Jeffrey, and Langley Research Center, eds. A users guide for the NASA ANOPP Propeller Analysis System: Under contract NAS1-96014. National Aeronautics and Space Administration, Langley Research Center, 1997.

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17

J, Kelly Jeffrey, and Langley Research Center, eds. A users guide for the NASA ANOPP Propeller Analysis System: Under contract NAS1-96014. National Aeronautics and Space Administration, Langley Research Center, 1997.

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18

Center, Lewis Research, ed. An estimate of the enroute noise of an advanced turboprop airplane. National Aeronautics and Space Administration, Lewis Research Center, 1986.

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19

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Annoyance caused by advanced turboprop aircraft flyover noise: Single-rotating propeller configuration. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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20

Center, Langley Research, ed. Annoyance caused by advanced turboprop aircraft flyover noise: Counter-rotating propeller configuration. National Aeronautics and Space Administration, 1990.

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21

A, Roussos Louis, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Consideration of some factors affecting low-frequency fuselage noise transmission for propeller aircraft. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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22

United States. National Aeronautics and Space Administration., ed. Cruise noise of counterrotation propeller at angle of attack in wind tunnel. National Aeronautics and Space Administration, 1987.

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23

Center, Langley Research, ed. The NASA Aircraft Noise Prediction Program improved Propeller Analysis System. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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24

J, Ranaudo Richard, Woodward Richard P, and United States. National Aeronautics and Space Administration., eds. In-flight measurement of propeller noise on the fuselage of an airplane. National Aeronautics and Space Administration, 1989.

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25

Heidelberg, Laurence J. Unsteady blade pressure measurements for the SR-7A propeller at cruise conditions. National Aeronautics and Space Administration, 1991.

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26

M, Tarkenton G., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Users' manual for the Langley high speed propeller noise prediction program (DFP-ATP). National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

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27

United States. National Aeronautics and Space Administration., ed. Aeroacoustics of advanced propellers. NASA, 1990.

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28

J, Loeffler Irvin, and United States. National Aeronautics and Space Administration., eds. In-flight near- and far-field acoustic data measured on the propfan test assessment (PTA) testbed and with an adjacent aircraft. National Aeronautics and Space Administration, 1993.

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29

J, Loeffler Irvin, and United States. National Aeronautics and Space Administration., eds. In-flight near- and far-field acoustic data measured on the propfan test assessment (PTA) testbed and with an adjacent aircraft. National Aeronautics and Space Administration, 1993.

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30

J, Loeffler Irvin, and United States. National Aeronautics and Space Administration., eds. In-flight near- and far-field acoustic data measured on the propfan test assessment (PTA) testbed and with an adjacent aircraft. National Aeronautics and Space Administration, 1993.

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31

J, Loeffler Irvin, and United States. National Aeronautics and Space Administration., eds. In-flight near- and far-field acoustic data measured on the propfan test assessment (PTA) testbed and with an adjacent aircraft. National Aeronautics and Space Administration, 1993.

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32

Valtion teknillinen tutkimuskeskus. Laivatekniikan laboratorio., ed. Pressure and noise induced by a cavitating marine screw propeller. Valtion teknillinen tutkimuskeskus, 1992.

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33

United States. National Aeronautics and Space Administration., ed. Aeroacoustic diffraction and dissipation by a short propeller cowl in subsonic flight. National Aeronautics and Space Administration, 1993.

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34

Powell, Clemans A. Potential subjective effectiveness of active interior noise control in propeller airplanes. National Aeronautics and Space Administration, Langley Research Center, 2000.

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35

Dunn, M. H. Computational methods in the prediction of advanced subsonic and supersonic propeller induced noise - ASSPIN users' manual. Langley Research Center, 1992.

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36

Woodward, Richard P. Noise of a counterrotation propeller with simulated fuselage and support pylon at takeoff/approach conditions. National Aeronautics and Space Administration, 1989.

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37

G, Hall David, and United States. National Aeronautics and Space Administration., eds. Detailed noise measurements on the SR-7A propeller: Tone behavior with helical tip Mach number. National Aeronautics and Space Administration, 1991.

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38

Center, Lewis Research, ed. Laboratory experiments on active suppression of advanced tuboprop noise. National Aeronautics and Space Administration, Lewis Research Center, 1985.

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39

Center, Langley Research, ed. Advanced turboprop aircraft flyover noise: Annoyance to counter-rotating-propeller configurations with a different number of blades on each rotor : preliminary results. National Aeronautics and Space Administration, Langley Research Center, 1988.

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40

Center, Langley Research, ed. Advanced turboprop aircraft flyover noise: Annoyance to counter-rotating-propeller configurations with an equal number of blades on each rotor : preliminary results. National Aeronautics and Space Administration, Langley Research Center, 1988.

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41

Center, Lewis Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. The radiation of sound from a propeller at angle of attack. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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42

Center, Langley Research, ed. Comparison of advanced turboprop and conventional jet and propeller aircraft flyover noise annoyance: Preliminary results. National Aeronautics and Space Administration, Langley Research Center, 1985.

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43

United States. National Aeronautics and Space Administration., ed. Potential reduction of en route noise from an advanced turboprop aircraft. National Aeronautics and Space Administration, 1990.

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44

P, Woodward Richard, Groeneweg John F, and United States. National Aeronautics and Space Administration., eds. High speed propeller performance and noise predictions at takeoff/landing conditions. National Aeronautics and Space Administration, 1988.

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45

P, Woodward Richard, Groeneweg J. F, and United States. National Aeronautics and Space Administration., eds. High speed propeller performance and noise predictions at takeoff/landing conditions. National Aeronautics and Space Administration, 1988.

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46

P, Gordon Eliott, and United States. National Aeronautics and Space Administration., eds. Noise of a model counterrotation propeller with reduced aft rotor diameter at simulated takeoff/approach conditions (F7/A3). National Aeronautics and Space Administration, 1987.

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47

B, Stang David, and United States. National Aeronautics and Space Administration., eds. Cruise noise of the 2/9th scale model of the large-scale advanced propfan (LAP) propeller, SR-7A. National Aeronautics and Space Administration, 1987.

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48

Center, Lewis Research, ed. Some design philosophy for reducing the community noise of advanced counter-rotation propellers. National Aeronautics and Space Administration, Lewis Research Center, 1985.

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49

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

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50

Center, Langley Research, ed. XV-15 low-noise terminal area operations testing. National Aeronautics and Space Administration, Langley Research Center, 1998.

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