Russian Aeronautics (Iz VUZ)

, Volume 53, Issue 1, pp 1–8

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

Authors

  • A. M. Girfanov
    • Tupolev State Technical University
  • V. V. Pavlov
    • Tupolev State Technical University
Flight Vehicle Design

DOI: 10.3103/S1068799810010010

Cite this article as:
Girfanov, A.M. & Pavlov, V.V. Russ. Aeronaut. (2010) 53: 1. doi:10.3103/S1068799810010010

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

Copyright information

© Allerton Press, Inc. 2010