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.
Mathematical model of balancing for a vertical takeoff and landing disk-wing aircraft
Russian Aeronautics (Iz VUZ) ; 53 , 1 ; 1-8
2010-03-01
8 pages
Article (Journal)
Electronic Resource
English
Mathematical model of balancing for a vertical takeoff and landing disk-wing aircraft
Online Contents | 2010
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