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1

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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2

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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3

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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4

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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5

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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6

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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7

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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8

Center, Ames Research, ed. Dynamic analysis of rotor blade undergoing rotor power shutdown. National Aeronautics and Space Administration, Ames Research Center, 1990.

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9

Center, Ames Research, ed. Dynamic analysis of rotor blade undergoing rotor power shutdown. National Aeronautics and Space Administration, Ames Research Center, 1990.

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10

Paxson, Daniel E. A numerical model for dynamic wave rotor analysis. National Aeronautics and Space Administration, 1995.

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11

Paxson, Daniel E. A numerical model for dynamic wave rotor analysis. National Aeronautics and Space Administration, 1995.

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12

L, Walsh Joanne, Riley Michael F, and Langley Research Center, eds. Integrated aerodynamic/dynamic optimization of helicopter rotor blades. National Aeronautics and Space Administration, Langley Research Center, 1989.

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13

Paxson, D. E. A numerical model for dynamic wave rotor analysis. National Aeronautics and Space Administration, 1995.

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14

Kvaternik, Raymond G. Airframe structural dynamic considerations in rotor design optimization. National Aeronautics and Space Administration, Langley Research Center, 1989.

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15

Sreekanta, Murthy T., and Langley Research Center, eds. Airframe structural dynamic considerations in rotor design optimization. National Aeronautics and Space Administration, Langley Research Center, 1989.

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16

Feng, N. S. Programs for rotor dynamic analysis using transfer matrix method. School of Mechanical and Industrial Engineering, University of New South Wales, 1988.

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17

Termidi, Hisamuddin. Dynamic characteristics of cable bolts. Laurentian University, School of Engineering, 1986.

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18

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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19

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

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20

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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21

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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22

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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23

D, Tóth Klára Ph, and Pungor E, eds. Dynamic characteristics of ion-selective electrodes. CRC Press, 1988.

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24

M, Larosiliere Louis, ed. Passage-averaged description of wave rotor flow. U.S. Army Research Laboratory, Lewis Research Center, 1997.

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25

M, Larosiliere Louis, and NASA Glenn Research Center, eds. Passage-averaged description of wave rotor flow. National Aeronautics and Space Administration, Lewis Research Center, 1997.

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26

M, Larosiliere Louis, and NASA Glenn Research Center, eds. Passage-averaged description of wave rotor flow. National Aeronautics and Space Administration, Lewis Research Center, 1997.

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27

M, Larosiliere Louis, and NASA Glenn Research Center, eds. Passage-averaged description of wave rotor flow. National Aeronautics and Space Administration, Lewis Research Center, 1997.

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28

Benton, Lau, and Ames Research Center, eds. Dynamics of the McDonnell Douglas large scale dynamic rig and dynamic calibration of the rotor balance. National Aeronautics and Space Administration, Ames Research Center, 1994.

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29

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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30

Passenger Car Meeting and Exposition (1990 Dearborn, Mich.). Dynamic characteristics of today's passenger car transmissions. Society of Automotive Engineers, 1990.

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31

L, Walsh Joanne, and Langley Research Center, eds. Integrated aerodynamic/dynamic/structural optimization of helicopter rotor blades using multilevel decomposition. National Aeronautics and Space Administration, Langley Research Center, 1995.

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32

Murthy, V. R. Linear and nonlinear dynamic analysis of redundant load path bearingless rotor systems. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1994.

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33

L, Walsh Joanne, ed. Integrated aerodynamic/dynamic/structural optimization of helicopter rotor blades using multilevel decomposition. National Aeronautics and Space Administration, Langley Research Center, 1995.

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34

Chattopadhyay, Aditi. An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor blades. Langley Research Center, 1990.

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35

Center, Ames Research, ed. Linear and nonlinear dynamic analysis of redundant load path bearingless rotor systems. National Aeronautics and Space Administration, Ames Research Center, 1985.

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36

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

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37

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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38

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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39

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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40

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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41

L, Walsh Joanne, and Langley Research Center, eds. Multilevel decomposition approach to integrated aerodynamic/dynamic/structural optimization of helicopter rotor blades. National Aeronautics and Space Administration, Langley Research Center, 1994.

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42

Flowers, G. T. Dynamic behavior of a magnetic bearing supported jet engine rotor with auxiliary bearings. TSI Press, 1994.

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43

Center, Ames Research, and United States. Army Aviation Research and Technology Activity., eds. A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor. NASA Ames Research Center, 1990.

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44

Takahashi, Marc D. A flight-dynamic helicopter mathematical model with a single flap-lag-torsion main rotor. NASA Ames Research Center, 1990.

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45

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

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46

Shen, Jun. Analysis and Synthesis of Dynamic Systems with Positive Characteristics. Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-3880-8.

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47

Chance, Julian Edward. Structural fault detection employing linear and nonlinear dynamic characteristics. University of Manchester, 1996.

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48

Kelly, Carney, Gallardo V. C, and NASA Glenn Research Center, eds. Simulation of aircraft engine blade-out structural dynamics. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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49

STENNER, KAREN. The Authoritarian Dynamic. Cambridge University Press, 2005.

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50

STENNER, KAREN. The Authoritarian Dynamic. Cambridge University Press, 2005.

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