Mathematical model of balancing for a vertical takeoff and landing disk-wing aircraft
Flight Vehicle Design
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- Cite this article as:
- Girfanov, A.M. & Pavlov, V.V. Russ. Aeronaut. (2010) 53: 1. doi:10.3103/S1068799810010010
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.
two-support torsion bar
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