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Books on the topic 'Rotor characteristics'

Author: Grafiati

Published: 28 May 2022

Last updated: 31 July 2025

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1

W, Elliott Joe, Orie Nettie M, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., United States. Army Aviation Systems Command., and Langley Research Center, eds. Rotor performance characteristics from an aeroacoustic helicopter wind-tunnel test program. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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2

Lewicki, David G. Vibration characteristics of OH-58A helicopter main rotor transmission. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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3

Piatak, David J. Stiffness characteristics of composite rotor blades with elastic couplings. National Aeronautics and Space Administration, 1997.

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4

W, Nixon Mark, Kosmatka J. B, and Langley Research Center, eds. Stiffness characteristics of composite rotor blades with elastic couplings. National Aeronautics and Space Administration, Langley Research Center, 1997.

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5

J, Coy John, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Vibration characteristics of OH-58A helicopter main rotor transmission. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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6

D, Hathaway Michael, United States. National Aeronautics and Space Administration., and United States. Army Aviation Systems Command., eds. Rotor wake characteristics of a transonic axial flow fan. National Aeronautics and Space Administration, 1986.

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7

L, Peterson Randall, Graham T. A, and Ames Research Center, eds. Simulated rotor test apparatus dynamic characteristics in the 80- by 120-foot wind tunnel. National Aeronautics and Space Administration, Ames Research Center, 1990.

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8

Hoad, Danny R. Rotor performance characteristics from an aeroacoustics helicopter wind-tunnel test program. Langley Research Center, 1986.

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9

Center, Ames Research, and United States. Army Aviation Research and Technology Activity., eds. Frequency-response identification of XV-15 tilt-rotor aircraft dynamics. National Aeronautics and Space Administration, Ames Research Center, 1987.

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10

Center, Ames Research, and United States. Army Aviation Research and Technology Activity., eds. Frequency-response identification of XV-15 tilt-rotor aircraft dynamics. National Aeronautics and Space Administration, Ames Research Center, 1987.

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11

Center, Ames Research, and United States. Army Aviation Research and Technology Activity., eds. Frequency-response identification of XV-15 tilt-rotor aircraft dynamics. National Aeronautics and Space Administration, Ames Research Center, 1987.

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12

G, Bousman William, and Ames Research Center, eds. Aerodynamic limitations of the UH-60A rotor. National Aeronautics and Space Administration, Ames Research Center, 1996.

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13

United States. National Aeronautics and Space Administration., ed. Blockage development in a transonic, axial compressor rotor. National Aeronautics and Space Administration, 1997.

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14

United States. National Aeronautics and Space Administration., ed. Blockage development in a transonic, axial compressor rotor. National Aeronautics and Space Administration, 1997.

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15

Lake, Renee C. Experimental and analytical investigation of dynamic characteristics of extension-twist-coupled composite tubular spars. Langley Research Center, 1993.

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16

E, Paxson D., Schobeiri M. T, and United States. National Aeronautics and Space Administration., eds. Dynamic simulation of a wave rotor topped turboshaft engine. National Aeronautics and Space Administration, 1997.

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17

Madsen, Helge Aagaard. Measured Airfoil Characteristics of Three Blade Segments on a 19 M Hawt Rotor. Riso National Laboratory, 1990.

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18

Larvin, Paul. Static testing and modelling of a small turbine rotor to identify its vibration characteristics. The Polytechnic, 1990.

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19

T, Flowers George, Trent Victor S, and United States. National Aeronautics and Space Administration., eds. Dynamic modelling and response characteristics of a magnetic bearing rotor system including auxiliary bearings. National Aeronautics and Space Administration, 1993.

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20

Corrigan, Robert D. Performance and power regulation characteristics of two aileron-controlled rotors and a pitchable tip-controlled rotor on the Mod-O wind turbine. U.S. Dept. of Energy, Conservation and Renewable Energy, Wind/Ocean Technology Division, 1987.

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21

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Aerodynamic characteristics of a rotorcraft airfoil designed for the tip region of a main rotor blade. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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22

Newman, Frederick A. Experimental vibration damping characteristics of the third-stage rotor of a three-stage transonic axial-flow compressor. National Aeronautics and Space Administration, 1988.

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23

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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24

United States. National Aeronautics and Space Administration., ed. Turbulent inflow measurements: Final report, grant number L-1625, period covered: 5 July 1995 to 31 December 1996. National Aeronautics and Space Administration, 1996.

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25

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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26

W, Kohlhepp F., Leighton K. P, and Ames Research Center, eds. Acoustic characteristics of 1/20-scale model helicopter rotors. Research Institute for Advanced Computer Science, NASA Ames Research Center, 1986.

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27

L, Cross Jeffrey, Noonan Kevin W, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

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28

L, Cross Jeffrey, Noonan Kevin W, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

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29

L, Cross Jeffrey, Noonan Kevin W, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

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30

Watts, Michael E. Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil. Ames Research Center, 1988.

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31

Christie, Agatha. El Espejo roto. Planeta-De Agostini, 1993.

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32

1939-, Okiishi T. H., and United States. National Aeronautics and Space Administration., eds. Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance. National Aeronautics and Space Administration, 1996.

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33

National Aeronautics and Space Administration (NASA) Staff. Tip Vortex and Wake Characteristics of a Counterrotating Open Rotor. Independently Published, 2019.

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34

Performance Analysis on Wear and Friction Characteristics of Brake Rotor Made of A359-B4c Composites. ASDF International, 2017.

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35

Exploratory flow visualization investigation of mast-mounted sights in presence of a rotor. National Aeronautics and Space Administration, Langley Research Center, 1995.

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36

Cost characteristics of tilt-rotor, conventional air and high speed rail short-haul intercity passenger service: Final report. Powered Lift Flight Investigation Branch, National Aeronautics and Space Administration, Ames Research Center, 1985.

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37

Cost characteristics of tilt-rotor, conventional air and high speed rail short-haul intercity passenger service: Final report. Powered Lift Flight Investigation Branch, National Aeronautics and Space Administration, Ames Research Center, 1985.

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38

Vaez-Zadeh, Sadegh. Introduction. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198742968.003.0001.

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Abstract:

An overview of permanent magnet synchronous (PMS) motors and the related control system are presented in this chapter as introductory materials for the rest of the book. The interconnections of the control system to the power electronic inverter and the motor are emphasized. In addition, the major parts of the system are overviewed. Pulse width-modulated voltage source inverter, as the most commonly used power converter in PMS motor drives, is briefly discussed. PMS motors configurations and operating principles are also presented after considering characteristics of permanent magnet materials

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39

Roter, Debra L., Sarina R. Isenberg, and Lauren M. Czaplicki. The Roter Interaction Analysis System. Oxford University Press, 2017. http://dx.doi.org/10.1093/med/9780198736134.003.0065.

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Abstract:

This chapter provides an introduction to the Roter Interaction Analysis System (RIAS) and reviews a selected body of studies that have used the system to describe cancer communication processes in a variety of cancer and palliative care contexts. It addresses a broad array of research questions relevant to the delivery of high-quality patient care, while providing a broad overview of the characteristics of the RIAS. Its contribution to the field of cancer communication is illustrated in this chapter by reviewing a selected body of cancer and palliative care studies that have used the RIAS as t

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40

El espejo roto. Planeta, 1994.

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41

Christie, Agatha. Espejo Roto, El. Planeta, 2000.

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