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1

Brooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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2

Brooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. Langley Research Center, 1988.

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3

Ralph, Jolly J., Marcolini Michael A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Helicopter main-rotor noise: Determination of source contributions using scaled model data. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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4

Brooks, Thomas F. Helicopter main-rotor noise: Determination of source contributions using scaled model data. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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5

Wilbur, Matthew L. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. National Aeronautics and Space Administration, Langley Research Center, 1998.

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6

Center, Langley Research, ed. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. National Aeronautics and Space Administration, Langley Research Center, 1998.

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7

Center, Langley Research, ed. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. National Aeronautics and Space Administration, Langley Research Center, 1998.

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8

Center, Langley Research, ed. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. National Aeronautics and Space Administration, Langley Research Center, 1998.

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9

Center, Langley Research, ed. Development of a rotor-body coupled analysis for an active mount aeroelastic rotor testbed. National Aeronautics and Space Administration, Langley Research Center, 1998.

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10

Coleman, Colin P. A survey of theoretical and experimental coaxial rotor aerodynamic research. National Aeronautics and Space Administration, 1997.

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11

Center, Ames Research, ed. A survey of theoretical and experimental coaxial rotor aerodynamic research. National Aeronautics and Space Administration, Ames Research Center, 1997.

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12

Center, Ames Research, ed. A survey of theoretical and experimental coaxial rotor aerodynamic research. National Aeronautics and Space Administration, Ames Research Center, 1997.

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13

R, Johnson Wayne, and United States. National Aeronautics and Space Administration., eds. Navier-Stokes calculations for a highly-twisted rotor near stall. National Aeronautics and Space Administration, 1994.

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14

E, Teske Milton, Quackenbush Todd R, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., and Ames Research Center, eds. A new methodology for free wake analysis using curved vortex elements. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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15

R, Johnson Wayne, and United States. National Aeronautics and Space Administration., eds. Navier-Stokes calculations for a highly-twisted rotor near stall. National Aeronautics and Space Administration, 1994.

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16

R, Johnson Wayne, and United States. National Aeronautics and Space Administration., eds. Navier-Stokes calculations for a highly-twisted rotor near stall. National Aeronautics and Space Administration, 1994.

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17

Runyan, Harry L. Compressible, unsteady lifting-surface theory for a helicopter rotor in forward flight. NASA, 1985.

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18

H, Tai, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Compressible, unsteady, lifting-surface theory for a helicopter rotor in forward flight. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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19

Pavlović, Momčilo. Rotari klub Subotica: 1929-1941, 1997-2008 = Szabadkai Rotary Klub = Szabadkai Rotary Klub. Rotari klub, 2008.

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20

Martin, R. M. Acoustic test of a model rotor and tail rotor: Results for the isolated rotors and combined configuration. National Aeronautics and Space Administration, Langley Research Center, 1989.

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21

Center, Ames Research, ed. A study of rotor broadband noise mechanisms and helicopter tail rotor noise. National Aeronautics and Space Administration, Ames Research Center, 1990.

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22

Riley, M. J. Measurements of the performance of a helicopter swept tip rotor in flight. [s.n.], 1986.

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23

Robinson, Christopher S. Modeling and analysis of helicopter ground resonance utilizing symbolic processing and dynamic simulation software. Naval Postgraduate School, 1997.

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24

International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (3rd 1990 Honolulu, Hawaii). Rotating machinery--transport phenomena: Proceedings of the Third International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-3). Hemisphere Pub. Corp., 1992.

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25

International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (3rd 1990 Honolulu, Hawaii). Rotating machinery--dynamics: Proceedings of the Third International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-3). Hemisphere Pub. Corp., 1992.

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26

Egolf, T. Alan. A full potential analysis with realistic wake influence for helicopter rotor airload prediction. Ames Research Center, 1987.

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27

Kitaplioglu, Cahit. Analysis of small-scale rotor hover performance data. National Aeronautics and Space Administration, Ames Research Center, 1990.

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28

J, Mack, Mount R, and United States. National Aeronautics and Space Administration., eds. Two rotor stratified charge rotary engine (SCRE) engine system technology evaluation. National Aeronautics and Space Administration, 1994.

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29

Hamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. Ames Research Center, 1990.

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30

Hamade, Karen S. Modal analysis of UH-60A instrumented rotor blades. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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31

M, Kufeld Robert, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Modal analysis of UH-60A instrumented rotor blades. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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32

M, Kufeld Robert, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Modal analysis of UH-60A instrumented rotor blades. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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33

United States. National Aeronautics and Space Administration., ed. Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight: An experimental and analytical investigation of isolated rotor-flap-lag stability in forward flight. Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering, 1986.

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34

United States. National Aeronautics and Space Administration., ed. Toward comparing experiment and theory for corroborative research on hingeless rotor stability in forward flight: Final technical report under NASA-Ames cooperative agreement no. NCC 2-361 (August 1, 1985 - July 31, 1987). Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering, 1987.

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35

Khánh, Nguyẽ̂n, and Ames Research Center, eds. Aeroelastic stability of a full-scale hingeless rotor. National Aeronautics and Space Administration, Ames Research Center, 1996.

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36

Khanh, Nguyen, and Ames Research Center, eds. Aeroelastic stability of a full-scale hingeless rotor. National Aeronautics and Space Administration, Ames Research Center, 1996.

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37

Kadiĭski, T︠S︡vi︠a︡tko. Rotari v Sofii︠a︡: Legenda i deĭstvitelnost. Kolbis, 2000.

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38

Rosenstein, H. Aerodynamic development of the V-22 tilt rotor. [s.n.], 1986.

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39

Rosenstein, H. Aerodynamic development of the V-22 tilt rotor. AIAA, 1986.

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40

Peretz, Friedmann, and Ames Research Center, eds. Aeroelastic simulation of higher harmonic control. National Aeronautics and Space Administration, Ames Research Center, 1994.

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41

P, Friedmann Peretz, and Ames Research Center, eds. Aeroelastic simulation of higher harmonic control. National Aeronautics and Space Administration, Ames Research Center, 1994.

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42

Chen, Robert T. N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. National Aeronautics and Space Administration, Ames Research Center, 1990.

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43

Chen, Robert T. N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. Ames Research Center, 1989.

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44

Center, Ames Research, ed. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. National Aeronautics and Space Administration, Ames Research Center, 1993.

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45

S, Childress Otis, Hardesty Mark, and Langley Research Center, eds. Helicopter main-rotor speed effects on far-field acoustic levels. National Aeronautics and Space Administration, Langley Research Center, [Springfield, Va., 1987.

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46

Fejtek, Ian G. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. Ames Research Center, 1993.

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47

S, Childress Otis, Hardesty Mark, and Langley Research Center, eds. Helicopter main-rotor speed effects on far-field acoustic levels. National Aeronautics and Space Administration, Langley Research Center, [Springfield, Va., 1987.

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48

1936-, Tung C., and Ames Research Center, eds. Performance and pressure data from a small model tilt-rotor in hover. National Aeronautics and Space Administration, Ames Research Center, 1997.

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49

S, Childress Otis, Hardesty Mark, and Langley Research Center, eds. Helicopter main-rotor speed effects on far-field acoustic levels. National Aeronautics and Space Administration, Langley Research Center, [Springfield, Va., 1987.

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50

Center, Ames Research, ed. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover. National Aeronautics and Space Administration, Ames Research Center, 1993.

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