Mathematical model of balancing for a vertical takeoff and landing disk-wing aircraft
Flight Vehicle Design
- 78 Downloads
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 wordsdisk wing disk-wing aircraft balancing mathematical model two-support torsion bar
Unable to display preview. Download preview PDF.
- 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.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.Johnson, Wayne, Helicopter Theory, Princeton: Princeton University Press, 1980.Google Scholar
© Allerton Press, Inc. 2010