Zobrazeno 1 - 5
of 5
pro vyhledávání: '"K. O. Chernigin"'
Publikováno v:
Научный вестник МГТУ ГА, Vol 27, Iss 4, Pp 20-33 (2024)
During the operation of single-rotor helicopters, aviation accidents quite frequently occur in the form of an unintentional turn or even a yaw rotation, causing, as a rule, a ground collision. Numerous researchers of this problem consider the loss of
Externí odkaz:
https://doaj.org/article/9a30f5cd12044378aabf7ef0add7e731
Publikováno v:
Научный вестник МГТУ ГА, Vol 23, Iss 2, Pp 33-46 (2020)
Aviation accidents related to unintentional rotation may periodically occur while flying single-rotor helicopters. On-time and correct actions may help the pilot to find the way out of this hazardous situation. But it is also important to understand
Externí odkaz:
https://doaj.org/article/3c260698de6244a9a6b894c0b2ec3550
Autor:
V. V. Efimov, K. O. Chernigin
Publikováno v:
Научный вестник МГТУ ГА, Vol 21, Iss 1, Pp 185-194 (2018)
Functional properties characterize the purpose of the aircraft and are described by its flight performance characteristics such as range and cruising speed, payload, runway characteristics, etc. Functional properties also characterize the aircraft ef
Externí odkaz:
https://doaj.org/article/ba5bb647bc44483d9d75059cb6446ce9
Autor:
V. V. Efimov, K. O. Chernigin
Publikováno v:
Научный вестник МГТУ ГА, Vol 19, Iss 6, Pp 24-34 (2017)
Aircraft are high-tech engineering products which are characterized by a wide range of properties including the two most important groups that respectively characterize the efficiency and technical level.Improving the aircraft efficiency is an essent
Externí odkaz:
https://doaj.org/article/11fc20db269a4629bd4e59b673383e3d
Autor:
M. S. Kublanov, K. O. Chernigin
Publikováno v:
Научный вестник МГТУ ГА, Vol 19, Iss 6, Pp 35-41 (2017)
Based on the information from the Internet the authors decided to reproduce the possible conditions of landing the plane IL-76TD-90VD in Antarctica in their computer experiment using the mathematical modeling system of aircraft flight dynamics (MMS A
Externí odkaz:
https://doaj.org/article/78d437ff3df94697a2058db86b77da85