| Шығарылым |
Атауы |
Файл |
| Том 62, № 3 (2019) |
3D Investigation of Film Cooling Effectiveness for Nozzle Vane Platform of High Pressure Turbine with “Meridian Constriction” and Laidback Fan-Shaped Film-Cooling Holes |
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Gorelov Y.
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| Том 61, № 3 (2018) |
3D Investigations of the High Pressure Turbine Vane Platform Convection Cooling and Convection-Film Cooling |
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Gorelov Y., Anan’ev V.
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| Том 59, № 4 (2016) |
A combined method for calculating the trajectories of suspended particles |
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Zaripov T., Gil’fanov A.
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| Том 59, № 4 (2016) |
A combined model of calculating the durability of aircraft engine high speed rolling bearings |
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Silaev B., Danilenko P.
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| Том 61, № 1 (2018) |
A Computational Technique for Estimating the Nitrogen Oxide Concentration in Combustion of Air-Fuel Mixture Enriched with Hydrogen in Exhaust Gases of Spark-Ignition Engines |
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Shaikin A., Ivashin P., Deryachev A.
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| Том 59, № 1 (2016) |
A high-temperature frameless starter-generator integrated into an aircraft engine |
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Ismagilov F., Khairullin I., Vavilov V., Farrakhov D., Yakubov A., Bekuzin V.
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| Том 59, № 4 (2016) |
A mathematical model of transforming the vertical takeoff and landing aircraft with a disk wing at maneuvering (on a deck) |
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Pavlov V.
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| Том 61, № 2 (2018) |
A Method for Designing the Helicopter Skid Landing Gear by a Criterion of Landing Impact Energy Absorption |
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Nedel’ko D., Alimov S.
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| Том 62, № 4 (2019) |
A Method for Express Analysis of Mechanical, Erosion, and Contaminating Impact of Plasma Jet of Electric Propulsion Thruster onto the Large Object of Space Debris |
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Blyakharskii S., Blyakharskii Y., Nadiradze A., Rakhmatullin R.
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| Том 62, № 3 (2019) |
A Method of Calculating the Small-Sized Combustion Chambers |
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Lanskii A., Lukachev S., Matveev S., Kolomzarov O.
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| Том 59, № 4 (2016) |
A method of design calculation for the two-component jet-jet gas nozzle with outer mixing |
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Egorychev V., Ryazanov A.
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| Том 60, № 3 (2017) |
A method of determining the aircraft motion parameters at landing |
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Larionov V.
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| Том 61, № 1 (2018) |
A Method of Working Process Parameter Optimization of a Unified Engine Core and a Gas Turbine Engine Family Being Created on Its Basis |
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Rybakov V., Kuz’michev V., Tkachenko A., Krupenich I.
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| Том 62, № 4 (2019) |
A Method to Improve the Aircraft Aerodynamic Characteristics at High Angles of Attack and in Spin |
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Golovkin M., Gorbunov V., Efremov A., Drach D., Podobedov V.
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| Том 61, № 2 (2018) |
A Quasi-Spherical Air Pressure Probe |
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Golovkin M., Efremov A., Sysoev V.
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| Том 59, № 2 (2016) |
A simulator of the aircraft air data system |
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Efremova E.
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| Том 60, № 1 (2017) |
A technique for numerical modeling of liquid film disintegration in the pneumatic injector of aircraft engines |
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Kolodyazhnyi D., Nagornyi V., Sipatov A., Modorskii V.
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| Том 61, № 2 (2018) |
A Technique for Shortening Landing Run Distance of an Aircraft by Symmetrical Deflection of Split Elevator and Rudder |
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Bazuhair M.
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| Том 61, № 4 (2018) |
A Technique of Calculating a Load-Bearing Frame of Aircraft Passenger Seat Unit in Virtual Certification Tests |
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Shabalin L., Sidorov I., Khaliulin V., Gorelov A.
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| Том 59, № 4 (2016) |
A technique of finite element analysis for co-curing a composite shell with integral metal part |
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Shabalin L., Khilov P., Sungatullin R.
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| Том 60, № 1 (2017) |
A technique of gaseous fuel and air mixture quality identification behind the swirl burner of gas turbine engine combustion chamber |
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Baklanov A., Neumoin S.
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| Том 60, № 4 (2017) |
A Technique of Holes Axes Definition in Hidden and Hard-to-Get-to Hardware Zones by Means of Laser Coordinate Measuring Systems |
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Lyudogovskii P., Komkova M.
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| Том 60, № 4 (2017) |
A Technique of Object Detection Using Information about Changes in the Terrain Image |
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Miftakhutdinov D., Rizaev I., Shleimovich M.
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| Том 62, № 4 (2019) |
A Wheel Motor for Aircraft Application |
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Afanas’ev A., Karimov A., Studneva E.
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| Том 62, № 2 (2019) |
About Optimal Reception of Pseudorandom Signals of Nonlinear Dynamic Systems |
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Nasyrov I., Andreev V.
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| Нәтижелер 410 - 1/25 |
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