| Шығарылым |
Атауы |
Файл |
| Том 59, № 3 (2016) |
Calculation and optimization of aerodynamic characteristics of airfoils with jet blowing in the presence of vortex in the flow |
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Abzalilov D., Mardanov R.
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| Том 61, № 4 (2018) |
Calculation Methods for Estimating the Rotary Derivatives of Forces and Moments Acting on the Aircraft |
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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 |
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Gorelov A., Nikolaev E., Sidorov I.
|
| Том 59, № 1 (2016) |
Calculation of design relative density for rational sandwich structure with truss core |
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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 |
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Kochetkov Y., Molchanov A., Siluyanova M.
|
| Том 62, № 3 (2019) |
Calculation of Labor Intensity in the Context of Pilot Production of Small Aircraft |
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Sharafeev I., Markovtsev V.
|
| Том 60, № 3 (2017) |
Calculation of low cycle fatigue life for gas-turbine engine critical parts |
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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 |
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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 |
|
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Baklanov A., Malyukov A.
|
| Том 62, № 1 (2019) |
Changes in the Cruise Climb Performance of the Il-96-300 Aircraft |
|
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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 |
|
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Emel’yanova Y., Khachumov V.
|
| Том 59, № 2 (2016) |
Collapse of a spheroidal cavitation bubble near a solid wall |
|
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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 |
|
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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 |
|
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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 |
|
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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 |
|
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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 |
|
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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 |
|
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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 |
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Soldatkin V., Nikitin A.
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| Нәтижелер 410 - 76/100 |
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