Zobrazeno 1 - 10
of 19
pro vyhledávání: '"I. K. Turkin"'
Autor:
A. I. Selin, I. K. Turkin
Publikováno v:
Научный вестник МГТУ ГА, Vol 26, Iss 2, Pp 91-105 (2023)
Currently, the big number of companies, and specifically in Russia, is engaged in designing unmanned aerial vehicles (UAV). It is caused by the tendency to reduce human labor in various fields of activity, in particular, associated with a great risk
Externí odkaz:
https://doaj.org/article/4622e7dd2d694eaab7e29255a8f9f53e
Publikováno v:
Научный вестник МГТУ ГА, Vol 24, Iss 4, Pp 61-74 (2021)
The article investigates the problem of hydro-elastic interaction of a weak shock wave with a rigid nosed rotation shell preloaded with axial forces. The shell is enclosed in a rigid parabolic screen, i.e. the impact of the end face and the shock wav
Externí odkaz:
https://doaj.org/article/5e998e1280e34dc484f825255a034f00
Publikováno v:
Научный вестник МГТУ ГА, Vol 20, Iss 4, Pp 162-173 (2017)
The notion of “the concept on assumed risk” that took over from the outdated concept of absolute security is analyzed, the increasing significance of operating risk assessment at the present stage is noted. Some basic risk assessment techniques a
Externí odkaz:
https://doaj.org/article/50e505efd2f4479aaf983fe4266ab86f
Autor:
I. K. Turkin, D. A. Rogov
Publikováno v:
Научный вестник МГТУ ГА, Vol 20, Iss 3, Pp 122-130 (2017)
At the present stage of aviation and missile equipment development there is increasing necessity for considering fast-acting, high-speed processes of impact interaction of structure elements with external loads, represented as both power factors (lon
Externí odkaz:
https://doaj.org/article/e9e61e2f64c8423ebfc2a8a574149d68
Autor:
I. K. Turkin, D. A. Rogov
Publikováno v:
Научный вестник МГТУ ГА, Vol 0, Iss 225, Pp 166-172 (2016)
The article deals with the dynamic behavior of the unevenly heated thin-walled conical shell of revolution of the aircraft fairing type under the loading conditions by shock wave in the gaseous environment, approximated by travelling load. The displa
Externí odkaz:
https://doaj.org/article/3737dbcc1b7a4fc9a0d14a4d5d92c89f
Autor:
D. A. Trokhov, I. K. Turkin
Publikováno v:
Научный вестник МГТУ ГА, Iss 221, Pp 106-114 (2016)
The method of optimal technical configuration synthesis and selection of long flight duration unmanned aerial vehicles are presented herein. Problems of mission effectiveness, take-off weight, aerodynamic and power plant characteristics calculations
Externí odkaz:
https://doaj.org/article/881907dc68f646a0be5d442fb7179c25
Autor:
I. K. Turkin
Publikováno v:
Russian Aeronautics. 65:156-164
Autor:
S. G. Parafes, I. K. Turkin
Publikováno v:
Russian Aeronautics. 63:75-82
An approach to design of the rudder—drive system taking into account the aeroelastic characteristics of the rudder is proposed. Mathematical models are developed that are used to solve problems of the rudder design parameters selection and the rudd
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). 59:331-337
Theoretical and experimental methods of investigating the performance of an electric actuator of maneuverable unmanned aerial vehicle (UAV) is considered in order to solve the aeroelasticity tasks. Models of the stability analysis for the rudder–ac