Zobrazeno 1 - 3
of 3
pro vyhledávání: '"M. S. Makhnev"'
Publikováno v:
Научный вестник МГТУ ГА, Vol 19, Iss 6, Pp 102-109 (2017)
This paper presents the initial stage of work out of the helicopter body aerodynamic configuration. The main purpose of this work is to design the model of the fuselage and to minimize its drag.The analysis of experimental data obtained in TsAGI and
Externí odkaz:
https://doaj.org/article/309a6fef2a414096ba3667c17778de50
AERODYNAMIC CHARACTERISTICS CALCULATION ON SINGLE ROTOR BLADE USING FLOEFD, ANSYS FLUENT AND RC-VTOL
Publikováno v:
Научный вестник МГТУ ГА, Iss 223, Pp 77-83 (2016)
The results of computational simulation of helicopter rotor's single blade flow, for which experimental (model test) data are published, are represented in this article. The calculations were made in the universal software package of CFD modeling Flo
Externí odkaz:
https://doaj.org/article/c08d476ba6844fe39441268aae4f62fb
Publikováno v:
Russian Aeronautics. 61:547-554
In order to determine the rotary derivatives of forces and moments with respect to the angular velocity components, a method of their estimation is developed based on calculations of distributed static aerodynamic characteristics of aircraft under th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::492952ed245e8d9200b7bceb9f87872e
https://doi.org/10.3103/s1068799818040074
https://doi.org/10.3103/s1068799818040074