Skip to main content
Article thumbnail
Location of Repository

Helicopter tail rotor instability

By A. Champneys
Topics: Aerospace and defence
Year: 2003
OAI identifier: oai:generic.eprints.org:25/core70

Suggested articles

Citations

  1. (1970). [11] Stammers C.W., The Flutter of a Helicopter Rotor Blade in Forward Flight, The Aeronautical Quarterly,
  2. (1975). A Bifurcation Method to Calculate Flutter Characteristics of a Helicopter Blade having Complex Damping,
  3. (2003). Further Data from Simulation of Tail Rotor Private Communication (fax),
  4. (2002). Mathematical Model of a Helicopter Tail Rotor, Master of Engineering Project Thesis,
  5. (2000). Nonlinear Oscillations, Wiley 1979, [8] Krodkiewski J.M., Faragher J.S., Stabilization of Motion of Helicopter Rotor Blades using Delayed-Feedback Modelling, Computer Simulation and Experimental Verification,
  6. (1986). Numerical Methods for Determining the Stability and Response of Periodic Systems with Applications to Helicopter Rotor Dynamics and Aeroelasticity, Comp. and Maths. with Appls.,
  7. (1999). Periodic Flap Control of a Helicopter Blade in Forward Flight,
  8. (1998). Stability and Control of a Parametrically Excited Rotating System, Part I: Stability Analysis, Dynamics and Control,
  9. (1998). Stability and Control of a Parametrically Excited Rotating System, Part II: Controls, Dynamics and control,
  10. (2001). Stability of Simple Teetering Tail Rotor, Private Communication

To submit an update or takedown request for this paper, please submit an Update/Correction/Removal Request.