Мақалалар тізімі

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Том 59, № 3 (2016) Calculation and optimization of aerodynamic characteristics of airfoils with jet blowing in the presence of vortex in the flow
Abzalilov D., Mardanov R.
Том 61, № 4 (2018) Calculation Methods for Estimating the Rotary Derivatives of Forces and Moments Acting on the Aircraft
Golovkin M., Efremov A., Makhnev M., Setukha A.
Том 59, № 3 (2016) Calculation of a safety factor of damaged composite main rotor blade according to limit equilibrium theory
Gorelov A., Nikolaev E., Sidorov I.
Том 59, № 1 (2016) Calculation of design relative density for rational sandwich structure with truss core
Gainutdinov V., Abdullin I., Musavy-Safavy S.
Том 62, № 3 (2019) Calculation of High-Altitude Jets of the Rocket Engine Based on Quasi-Gasdynamic Equations
Kochetkov Y., Molchanov A., Siluyanova M.
Том 62, № 3 (2019) Calculation of Labor Intensity in the Context of Pilot Production of Small Aircraft
Sharafeev I., Markovtsev V.
Том 60, № 3 (2017) Calculation of low cycle fatigue life for gas-turbine engine critical parts
Pakhomenkov A., Azimov R., Bukatyi S.
Том 62, № 4 (2019) Calculation of Main Design Parameters of a Reactive Penetrator Intended for Movement in Lunar Soil
Zagovorchev V., Rodchenkov V.
Том 62, № 1 (2019) Calculation of the Fuel Gas Heating in the Flame Tube Head of Multi-Injector Combustion Chamber of the Gas Turbine Engine
Baklanov A., Malyukov A.
Том 62, № 1 (2019) Changes in the Cruise Climb Performance of the Il-96-300 Aircraft
Maslennikova G., Arep’ev K., Tazhetdinov R., Nikonov V., Spryskov V.
Том 61, № 1 (2018) Cognitive Graphical Additions to the Interfaces of Command Measurement Systems for Aerospace Application
Emel’yanova Y., Khachumov V.
Том 59, № 2 (2016) Collapse of a spheroidal cavitation bubble near a solid wall
Aganin A., Il’gamov M., Kosolapova L., Malakhov V.
Том 61, № 4 (2018) Comparative Analysis of Techniques of Modeling Kinematic Relations for Solving Helicopter Motion Equations
Girfanov A.
Том 60, № 3 (2017) Comparison of two configurations of a starter-generator integrated into the aircraft engine
Ismagilov F., Khairullin I., Vavilov V., Yakupov A.
Том 59, № 4 (2016) Composite model of a research flight simulator for a helicopter with the hingeless main rotor
Ledyankina O., Mikhailov S.
Том 60, № 2 (2017) Comprehensive approach to mathematical modeling and helicopter flight task optimization
Onushkin Y., Sizov D., Poluyakhtov V.
Том 60, № 3 (2017) Computation of design parameters influence on air injector fuel atomization
Sipatov A., Modorskii V., Babushkina A., Kolodyazhnyi D., Nagornyi V.
Том 59, № 1 (2016) Computational modeling of interference between helicopter main and tail rotors based on nonlinear blade vortex model
Ignatkin Y., Makeev P., Shomov A.
Том 61, № 3 (2018) Computational Research of the Main Rotor Hover and Vertical Descent States Based on the Nonlinear Blade Vortex Model
Ignatkin Y., Makeev P., Shaidakov V., Shomov A.
Том 62, № 2 (2019) Computational Research of the Main Rotor Steep Descent Modes Based on the Nonlinear Blade Vortex Model
Ignatkin Y., Makeev P., Shaidakov V., Shomov A.
Том 62, № 3 (2019) Computational Study of Interaction of Transverse Subsonic and Supersonic Axisymmetric Jets with Main Flow
Ziwan L., Varsegov V.
Том 59, № 3 (2016) Computationally effective mathematical model of airplane flight
Kudryavtsev D., Aminev D., Sviridov A.
Том 59, № 1 (2016) Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades
Kulikov G., Trushin V., Abdulnagimov A., Ganeev A.
Том 61, № 2 (2018) Concepts of Gas Turbine Engine Improvement Through the Use of Choked-Flow Turbines
Bogdanov V.
Том 60, № 3 (2017) Construction and algorithms of a helicopter air data system with aerometric and ion-tagging measurement channels
Soldatkin V., Nikitin A.
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