Book contents
- Frontmatter
- Contents
- Preface
- 1 Introduction
- 2 Notation
- 3 Hover
- 4 Vertical Flight
- 5 Forward Flight Wake
- 6 Forward Flight
- 7 Performance
- 8 Design
- 9 Wings and Wakes
- 10 Unsteady Aerodynamics
- 11 Actuator Disk
- 12 Stall
- 13 Computational Aerodynamics
- 14 Noise
- 15 Mathematics of Rotating Systems
- 16 Blade Motion
- 17 Beam Theory
- 18 Dynamics
- 19 Flap Motion
- 20 Stability
- 21 Flight Dynamics
- 22 Comprehensive Analysis
- Index
- References
19 - Flap Motion
Published online by Cambridge University Press: 05 May 2013
Book contents
- Frontmatter
- Contents
- Preface
- 1 Introduction
- 2 Notation
- 3 Hover
- 4 Vertical Flight
- 5 Forward Flight Wake
- 6 Forward Flight
- 7 Performance
- 8 Design
- 9 Wings and Wakes
- 10 Unsteady Aerodynamics
- 11 Actuator Disk
- 12 Stall
- 13 Computational Aerodynamics
- 14 Noise
- 15 Mathematics of Rotating Systems
- 16 Blade Motion
- 17 Beam Theory
- 18 Dynamics
- 19 Flap Motion
- 20 Stability
- 21 Flight Dynamics
- 22 Comprehensive Analysis
- Index
- References
Summary
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- Chapter
- Information
- Rotorcraft Aeromechanics , pp. 749 - 787Publisher: Cambridge University PressPrint publication year: 2013
References
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“Theory of Self-Excited Mechanical Oscillations of Hinged Rotor Blades.” NACA ARR 3G29, July 1943.Google Scholar
“Complex Coordinates in Near Hovering Rotor Dynamics.” Journal of Aircraft, 10:5 (May 1973).CrossRefGoogle Scholar
, and “A Stability and Control Theory for Hingeless Rotors.” American Helicopter Society 27th Annual National V/STOL Forum, Washington, DC, May 1971.Google Scholar
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“A Perturbation Solution of Helicopter Rotor Flapping Stability.” Journal of Aircraft, 10:5 (May 1973).CrossRefGoogle Scholar
“Perturbation Solutions for the Influence of Forward Flight on Helicopter Rotor Flapping Stability.” NASA TM 62361, August 1974.Google Scholar
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, and “Application of the Floquet Transition Matrix to Problems of Lifting Rotor Stability.” Journal of the American Helicopter Society, 16:2 (April 1971).CrossRefGoogle Scholar
“The Effect of Induced Velocity Variation on Helicopter Rotor Damping in Pitch or Roll.” ARC CP 101, November 1951.Google Scholar