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Russian Aeronautics

, Volume 61, Issue 1, pp 56–63 | Cite as

Dynamics of Main Rotor to Disk Wing Conversion

  • V. V. Pavlov
  • M. S. Gasilov
  • D. M. Yusupov
Aircraft and Rocket Engine Design and Development
  • 7 Downloads

Abstract

The accelerations that emerge in the disk wing during rotation have been found. The loading of wing elements have been determined when the blades are extended and retracted.

Keywords

disk wing dynamics flying saucer blade loads 

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References

  1. 1.
    Pavlov, V.A. and Pavlov, V.V., RU Patent no. 2101215, 1998.Google Scholar
  2. 2.
    Pavlov, V.A. and Pavlov, V.V., RU Patent no. 2192986, 2002.Google Scholar
  3. 3.
    Pavlov, V.A., RU Patent no. 2385267, 2010.Google Scholar
  4. 4.
    Pavlov, V.V., and Gasilov, M.S., Disk Wing to Main Rotor Conversion Mechanics, Izv. Vuz. Av. Tekhnika, 2016, vol. 59, no. 2, pp. 7–12 [Russian Aeronautics (Engl. Transl.), vol. 59, no. 2, pp. 161–167].Google Scholar
  5. 5.
    Pavlov, V.V., A Mathematical Model of Transforming the Vertical Takeoff and Landing Aircraft with a Disk Wing at Maneuvering (on a Deck), Izv. Vuz. Av. Tekhnika, 2016, vol. 59, no. 4, pp. 64–71 [Russian Aeronautics (Engl. Transl.), vol. 59, no. 4, pp. 507–516].Google Scholar
  6. 6.
    Pavlov, V.A., Geometrically Nonlinear Theory of Calculating Airfoil Rods, Izv.Vuz. Av. Tekhnika, 1981, vol. 24, no. 2, pp. 44–50 [Soviet Aeronautics (Engl. Transl.), vol. 24, no. 2].Google Scholar
  7. 7.
    Lur’e, A.I., Analiticheskaya mekhanika (The Analytic Mechanics), Moscow: Nauka, 1961.Google Scholar

Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  1. 1.Tupolev Kazan National Research Technical UniversityKazan TatarstanRussia

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