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15 - Mathematics of Rotating Systems

Published online by Cambridge University Press:  05 May 2013

Wayne Johnson
Wayne Johnson
Affiliation:
Aeromechanics Branch of NASA Ames Research Center
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Rotorcraft Aeromechanics , pp. 545 - 581
Publisher: Cambridge University Press
Print publication year: 2013

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References

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Chopra, I., and Sivaneri, N.T. “Aeroelastic Stability of Rotor Blades Using Finite Element Analysis.” NASA CR 166389, August 1982.Google Scholar
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Gessow, A. “Equations and Procedures for Numerically Calculating the Aerodynamic Characteristics of Lifting Rotors.” NACA TN 3747, October 1956.Google Scholar
Grodko, L.N. “Ground Resonance.” In Helicopter, Calculation and Design, Mil, M.L., et al. Moscow: Izdatel'stvo Mashinostroyeniye, 1966. Translation “Vibrations and Dynamic Stability”, NASA TT F-519, May 1968.Google Scholar
Hoffman, J.A. “A Multi-Blade Coordinate Transformation Procedure for Rotors with Two Blades.” Paragon Pacific Inc., Report PPI-1014-5, September 1976.Google Scholar
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Johnson, W. “Development of a Comprehensive Analysis for Rotorcraft. Part II – Aircraft Model, Solution Procedure, and Applications.” Vertica, 5:3 (1981).Google Scholar
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Peters, D.A., and Izadpanah, A.P. “Helicopter Trim by Periodic Shooting with Newton-Raphson Iteration.” American Helicopter Society 37th Annual Forum, New Orleans, LA, May 1981.Google Scholar
Tanner, W.H. “Charts for Estimating Rotary Wing Performance in Hover and at High Forward Speeds.” NASA CR 114, November 1964.Google Scholar
Young, M.I., and Lytwyn, R.T. “The Influence of Blade Flapping Restraint on the Dynamic Stability of Low Disk Loading Propeller-Rotors.” Journal of the American Helicopter Society, 12:4 (October 1967).CrossRefGoogle Scholar

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