Zobrazeno 1 - 6
of 6
pro vyhledávání: '"O. A. Zavalov"'
Publikováno v:
Russian Aeronautics. 61:32-36
The concept and definition of integrated flight performance for a small remotely piloted helicopter are introduced to obtain real operational values in performing a flight mission.
Publikováno v:
Russian Aeronautics (Iz VUZ). 57:349-352
The basic parameters of steering servo for a small remotely piloted single-rotor helicopter with tail rotor are determined.
Autor:
KUPRIKOV, Mikhail Yu.1 kuprikov@mai.ru, RABINSKIY, Lev N.2 rabinskiy@mail.ru, KUPRIKOV, Nikita M.2,3 nkuprikov@mai.ru
Publikováno v:
INCAS Bulletin. 2019 Special Issue, Vol. 11, p153-162. 10p.
Publikováno v:
Fluid Dynamics. May2016, Vol. 51 Issue 3, p419-433. 15p. 5 Diagrams, 1 Chart, 5 Graphs.
The Concept and Definition of Integrated Flight Performance for a Small Remotely Piloted Helicopter.
Publikováno v:
Russian Aeronautics; Jan2018, Vol. 61 Issue 1, p35-39, 5p
Publikováno v:
Russian Aeronautics; Oct2014, Vol. 57 Issue 4, p349-352, 4p