Vestnik Moskovskogo aviatsionnogo instituta
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Published By Moscow Aviation Institute (National Research University)

0869-6101
Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Thermal conductivity research of the aircraft heat-insulating skin under flight conditions

2021 ◽  
Vol 28 (4) ◽  
pp. 118-130
Author(s):  
Vladimir A. Maskaykin ◽  
Vladislav P. Makhrov
Keyword(s):  
Thermal Conductivity

Speed control channel automation while aircraft aerial refueling

2021 ◽  
Vol 28 (1) ◽  
pp. 137-146
Author(s):  
Angelina Chebakova ◽  
Oleg Ganyak ◽  
Oleg Tkachenko
Keyword(s):  
Speed Control ◽  
Control Channel ◽  
Aerial Refueling

Nitridation technology specifics of high-alloy corrosion-resistant steels of aviation purposes

2021 ◽  
Vol 28 (2) ◽  
pp. 206-215
Author(s):  
Petr Bibikov ◽  
Irina Belashova ◽  
Mikhail Prokof'ev
Keyword(s):  
High Alloy ◽  
Corrosion Resistant

Mathematical model identification of gas turbine engine with account for initial data uncertainty

2021 ◽  
Vol 28 (3) ◽  
pp. 171-185
Author(s):  
Oleg Baturin ◽  
Paul Nikolalde ◽  
Grigorii Popov ◽  
Anastssia Korneeva ◽  
Ivan Kudryashov
Keyword(s):  
Mathematical Model ◽  
Initial Data ◽  
Gas Turbine ◽  
Model Identification ◽  
Gas Turbine Engine ◽  
Data Uncertainty ◽  
Turbine Engine

Development of very low-power PlaS-type plasma thrusters

2021 ◽  
Vol 28 (1) ◽  
pp. 74-85
Author(s):  
Matvey Kaplin ◽  
Olga Mitrofanova ◽  
Mira Bernikova
Keyword(s):  
Low Power ◽  
Plasma Thrusters

Analysis of the external airbags application expediency on a helicopter

2021 ◽  
Vol 28 (2) ◽  
pp. 127-141
Author(s):  
Evgeny Nikolaev ◽  
Pavel Yugai

Flow swirl impact at the rocket engine nozzle inlet on the flow coefficient

2021 ◽  
Vol 28 (2) ◽  
pp. 142-151
Author(s):  
Ruslan Shaidullin ◽  
Albert Bekerov ◽  
Andrey Sabirzyanov
Keyword(s):  
Rocket Engine ◽  
Flow Coefficient ◽  
Flow Swirl ◽  
Nozzle Inlet
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