Russian Aeronautics (Iz VUZ)

, Volume 53, Issue 1, pp 1–8 | Cite as

Mathematical model of balancing for a vertical takeoff and landing disk-wing aircraft

  • A. M. Girfanov
  • V. V. Pavlov
Flight Vehicle Design
  • 78 Downloads

Abstract

Basic principles of a mathematical model for disk-wing aircraft balancing and evaluation of power expenditure for flight as compared with a helicopter are presented.

Key words

disk wing disk-wing aircraft balancing mathematical model two-support torsion bar 

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References

  1. 1.
    Girfanov, A.M., Aeroelastic Analysis and Balancing of a Single-Rotor Helicopter with the Hingeless Rotor, Cand. Sci. (Tech.) Dissertation, Kazan, 2000.Google Scholar
  2. 2.
    Pavlov, V.A., Mikhailov, S.A., and Gainutdinov, V.G., Theory of Large and Finite Beam Displacements, Izv. Vuz. Av. Tekhnika, 1985, vol. 28, no. 3, pp. 55–58 [Soviet Aeronautics (Engl.Transl.), vol. 28, no. 3, pp. 61–64].Google Scholar
  3. 3.
    Johnson, Wayne, Helicopter Theory, Princeton: Princeton University Press, 1980.Google Scholar

Copyright information

© Allerton Press, Inc. 2010

Authors and Affiliations

  • A. M. Girfanov
    • 1
  • V. V. Pavlov
    • 1
  1. 1.Tupolev State Technical UniversityKazanRussia

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