Books on the topic 'Rotari'

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1

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

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2

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

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3

Polazzo, Marco. Pietro Rotari: Pittore veronese del Settecento (1707-1762). Negrar (Verona): Il Segno, 1990.

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4

La vita quotidiana dei Longobardi ai tempi di re Rotari. Imola (Bologna): G. Angelini, 2007.

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5

Il Settecento a Verona: Tiepolo, Cignaroli, Rotari : la nobiltà della pittura. Cinisello Balsamo (Milano): Silvana, 2011.

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6

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

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7

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

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8

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. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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9

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

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10

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

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11

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. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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12

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

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13

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

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14

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

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15

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

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16

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

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17

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

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18

Weber, Gregor J. M. Pietro Graf Rotari in Dresden: Ein italienischer Maler am Hof König Augusts III. : Bestandskatalog anlässlich der Ausstellung im Semperbau, 9. November 1999-9. Januar 2000. Emstetten/Dresden: Edition Imorde, 1999.

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19

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

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20

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. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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21

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

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22

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

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23

Korea) Hanyang Rotʻari Kʻŭllŏp (Seoul. Hanyang Rotʻari Kʻŭllŏp 30-yŏnsa: Rotary Club of Hanyang thirty years of service. Seoul, Korea: Hanyang Rotʻari Kʻŭllŏp, 1985.

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24

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

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25

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). Washington: Hemisphere Pub. Corp., 1992.

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26

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). Washington: Hemisphere Pub. Corp., 1992.

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27

Beach, Bert Beverly. Rotating the world with Rotary: Personal diary of a visiting Rotarian. [Maryland?]: B.B. Beach, 1991.

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28

Kʻŭllŏp, Migŭm Rotʻari. Migŭm Rotʻari simnyŏnsa: History of Rotary for 10 years serviced in Migum, 1981--1991. Kyŏnggi-do Migŭm-si: Migŭm Rotʻari Kʻŭllŏp, 1991.

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29

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

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30

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

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31

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

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32

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

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33

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

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34

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

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35

Rotary: Poems. Cincinnati, OH: Word Press, 2004.

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36

Cooper, Fiona. Rotary Spokes. London, England: Brilliance Books, 1988.

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37

Dudaș, Vasile. Pavel Rotariu. Timișoara: Excelsior Art, 2002.

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38

Cooper, Fiona. Rotary spokes. London: Serpent's Tail, 1995.

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39

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

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40

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

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41

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. Boca Raton, FL: Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering, 1986.

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42

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). Boca Raton, FL: Florida Atlantic University, Dept. of Mechanical Engineering, School of Engineering, 1987.

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43

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

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44

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

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45

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

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46

United States. Army. Aerostructures Directorate. and Langley Research Center, eds. Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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47

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

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48

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

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49

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. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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50

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. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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