| Шығарылым |
Атауы |
Файл |
| Том 62, № 2 (2019) |
Construction and Algorithms of the Onboard System for Measuring the Helicopter Air Data and State of the Atmosphere with a Stationary Receiver, Ion-Mark and Aerometric Measurement Channels |
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Soldatkin V., Nikitin A., Ariskin E.
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| Том 61, № 2 (2018) |
Continuous Flight Safety Management Information System for a Group of Converging Aircraft |
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Goncharenko V., Lebedev G., Mikhailin D., Khakhulin G.
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| Том 61, № 4 (2018) |
Control of a Piezo Actuator to Adjust the Reflective Surface of the Space-Based Reflector |
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Kabanov S., Mitin F., Krivushov A., Ulybushev E.
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| Том 59, № 3 (2016) |
Control of flight vehicles with the adjustable center of mass |
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Afanas’ev V., Degtyarev G., Kiselev V., Meshchanov A.
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| Том 61, № 4 (2018) |
Control of the LED Thermal Parameters for Display and Lighting Systems of On-Board Equipment |
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Skulkin N., Faizullin R., Mal’tsev A.
|
| Том 60, № 1 (2017) |
Control quality improvement for aircraft engine technological manufacturing processes |
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Lyutov A., Ryabov Y., Polezin S.
|
| Том 59, № 2 (2016) |
Control synthesis for an unmanned helicopter with time-delay under uncertain external disturbances |
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Garkushenko V., Vinogradov S., Barakos G.
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| Том 60, № 1 (2017) |
Controlled separation of nanosatellites by means of the pulsed magnetic field |
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Glushchenkov V., Yusupov R.
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| Том 60, № 2 (2017) |
Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight |
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Dehaeze F., Barakos G., Garipova L., Kusyumov A., Mikhailov S.
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| Том 61, № 2 (2018) |
Critical Conditions of Thermal Explosion Considering Space-Temporal Nonlocality |
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Kudinov V., Eremin A., Kudinov I., Zhukov V.
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| Том 60, № 1 (2017) |
Cross-correlation function computing pattern in the FPGA architecture |
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Evdokimov Y., Zakharov V., Shalagin S.
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| Том 60, № 2 (2017) |
Cyclic folding of composite zigzag structures and calculating of equipment parameters |
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Khaliulin V.
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| Том 62, № 2 (2019) |
Definition of the Generation Instants in Time of the Running Shaft Resonant Flexural Vibrations by Means of Indicator Function of the Number of States of Dynamic System |
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Tukmakov A., Tukmakova N.
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| Том 61, № 3 (2018) |
Definition of Wingtip Devices Shape and Dimensions for a Subsonic Airliner |
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Gueraiche D., Popov S., Ryzhov Y.
|
| Том 61, № 4 (2018) |
Deformation of an Elongated Thin-Shell Structure with a Dynamically Fracturing Thermal Protection Coating |
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Antuf’ev B.
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| Том 62, № 3 (2019) |
Deformation of the Shell of the Cylindrical Cryogenic Tank during its Filling |
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Zarubin V., Zimin V., Kuvyrkin G.
|
| Том 61, № 1 (2018) |
Design and Experimental Analysis of Aircrew Design Parameters to Vertical Takeoff and Landing |
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Gainutdinova T., Gainutdinov V.
|
| Том 62, № 1 (2019) |
Design Features and Efficiency Analysis of the Aircraft Complex Air Data System with a Fixed Flush-Mounted Flow Receiver |
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Soldatkin V.
|
| Том 60, № 2 (2017) |
Design of gating systems in production of gas turbine engine blades |
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Smykov A., Moiseev V., Chumadin A.
|
| Том 60, № 4 (2017) |
Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System |
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Makhrov V., Sorokin V., Yur’ev A.
|
| Том 59, № 3 (2016) |
Determination of ingredient composition of atmospheric emissions of the turbojet engine combustion gases by the fine-structure spectroscopy |
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Moskalenko N., Misbakhov R., Bagautdinov I., Loktev N., Dodov I.
|
| Том 61, № 1 (2018) |
Determination of Slag Retention Ability of Gating Systems |
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Izotov V., Serebryakov S., Shatul’skii A.
|
| Том 62, № 1 (2019) |
Determination of the Folded Core Geometric Characteristics Based on a Flat-Faceted Elementary Module with Translational Symmetry Considering the Material Thickness |
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Semeshko M., Alekseev K., Zakiro I., Markovtsev V.
|
| Том 62, № 3 (2019) |
Developing the Mathematical Model of a Pilot in a Control Manual Preview Tracking Task |
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Efremov A., Tyaglik M., Tyaglik A., Irgaleev I.
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| Том 62, № 3 (2019) |
Development and Investigation of Mathematical Models of Thermoelastic Stresses and Strains in Production of Multilayer Structures of Spherical Shape for Aircraft |
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Akimov I., Tugov V., Akimov A.
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| Нәтижелер 410 - 101/125 |
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