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19 - Flap Motion

Published online by Cambridge University Press:  05 May 2013

Wayne Johnson
Affiliation:
Aeromechanics Branch of NASA Ames Research Center
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Publisher: Cambridge University Press
Print publication year: 2013

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References

Amer, K.B.Theory of Helicopter Damping in Pitch or Roll and a Comparison with Flight Measurements.” NACA TN 2136, October 1950.Google Scholar
Amer, K.B., and Gustafson, F.B.Charts for Estimation of Longitudinal-Stability Derivatives for a Helicopter Rotor in Forward Flight.” NACA TN 2309, March 1951.Google Scholar
Coleman, R.P.Theory of Self-Excited Mechanical Oscillations of Hinged Rotor Blades.” NACA ARR 3G29, July 1943.Google Scholar
Curtiss, H.C. Jr.Complex Coordinates in Near Hovering Rotor Dynamics.” Journal of Aircraft, 10:5 (May 1973).CrossRefGoogle Scholar
Curtiss, H.C. Jr., and Shupe, N.K.A Stability and Control Theory for Hingeless Rotors.” American Helicopter Society 27th Annual National V/STOL Forum, Washington, DC, May 1971.Google Scholar
Glauert, H., and Shone, G.The Disturbed Motion of the Blades of a Gyroplane.” A.R.C. 995, 1933.Google Scholar
Horvay, G.Rotor Blade Flapping Motion.” Quarterly of Applied Mathematics, 5:2 (July 1947).CrossRefGoogle Scholar
Johnson, W.A Perturbation Solution of Helicopter Rotor Flapping Stability.” Journal of Aircraft, 10:5 (May 1973).CrossRefGoogle Scholar
Johnson, W.Perturbation Solutions for the Influence of Forward Flight on Helicopter Rotor Flapping Stability.” NASA TM 62361, August 1974.Google Scholar
Leishman, J.G.Etienne Oehmichen: Scientist, Engineer and Helicopter Pioneer.” American Helicopter Society 62th Annual Forum, Phoenix, AZ, May 2006.Google Scholar
Miller, R.H.Helicopter Control and Stability in Hovering Flight.” Journal of the Aeronautical Sciences, 15:8 (August 1948).CrossRefGoogle Scholar
Peters, D.A., and Hohenemser, K.H.Application of the Floquet Transition Matrix to Problems of Lifting Rotor Stability.” Journal of the American Helicopter Society, 16:2 (April 1971).CrossRefGoogle Scholar
Sissingh, G.J.The Effect of Induced Velocity Variation on Helicopter Rotor Damping in Pitch or Roll.” ARC CP 101, November 1951.Google Scholar

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  • Flap Motion
  • Wayne Johnson
  • Book: Rotorcraft Aeromechanics
  • Online publication: 05 May 2013
  • Chapter DOI: https://doi.org/10.1017/CBO9781139235655.020
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  • Flap Motion
  • Wayne Johnson
  • Book: Rotorcraft Aeromechanics
  • Online publication: 05 May 2013
  • Chapter DOI: https://doi.org/10.1017/CBO9781139235655.020
Available formats
×

Save book to Google Drive

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Google Drive.

  • Flap Motion
  • Wayne Johnson
  • Book: Rotorcraft Aeromechanics
  • Online publication: 05 May 2013
  • Chapter DOI: https://doi.org/10.1017/CBO9781139235655.020
Available formats
×