Flight Vehicle Design

Russian Aeronautics (Iz VUZ)

, Volume 53, Issue 1, pp 1-8

First online:

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

  • A. M. GirfanovAffiliated withTupolev State Technical University
  • , V. V. PavlovAffiliated withTupolev State Technical University

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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