Шығарылым |
Атауы |
Файл |
Том 61, № 3 (2018) |
Analysis of Gas Dynamics and Combustion in a Small Reverse-Flow Combustion Chamber |
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Yousef W., Sychenkov V., Davydov N., Aleksandrov Y.
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Том 60, № 2 (2017) |
Analysis of hydrodynamic unsteady turbulent flow structure in an aircraft power plant channels |
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Kraev V., Myakochin A.
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Том 59, № 3 (2016) |
Analysis of innovative methods application for production of composite integral parts |
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Khaliulin V., Batrakov V.
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Том 60, № 4 (2017) |
Analysis of PID Controller Parameters Influence on Dynamic Properties of an Active Magnetic Suspension |
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Izosimova T., Evdokimov Y.
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Том 62, № 1 (2019) |
Analysis of Process Setting Accuracy for Multifunctional CNC-Machines |
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Yusupov Z.
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Том 59, № 1 (2016) |
Analysis of stress state in a root-airfoil transition zone of hollow wide chord fan blades |
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Berdin V., Smyslov A., Berdin N., Luk’yanov V.
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Том 60, № 1 (2017) |
Analysis of structural elements made of composite materials with defects |
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Kokurov A., Odintsev I.
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Том 62, № 4 (2019) |
Analysis of the Impact of Fan Blade Geometric Deviations on the Strength Properties |
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Arkhipov A., Volgina M., Matushkin A., Ravikovich Y., Kholobtsev D.
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Том 60, № 3 (2017) |
Analysis of the spacecraft vertical landing dynamics on the platform with crash legs |
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Shcheglov G., Lukovkin R.
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Том 60, № 1 (2017) |
Analytical and asymptotic solution of boundary value problems in the mechanics of deformed shells under concentrated loading |
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Bakulin V., Vinogradov Y.
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Том 59, № 1 (2016) |
Analytical construction of interception trajectories in atmosphere |
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Afanas’ev V., Degtyarev G., Meshchanov A.
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Том 62, № 2 (2019) |
Analytical Design of the Law for Control of the Center of Mass Motion for an Unmanned Aerial Vehicle |
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Afanas’ev V., Degtyarev G., Meshchanov A.
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Том 62, № 3 (2019) |
Analytical Evaluation of Box Wing Aircraft Aerodynamic Characteristics at Early Design Stages |
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Karpovich E., Liseitsev N.
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Том 62, № 3 (2019) |
Analytical Synthesis of a Modal Controller by Output Vector for Attitude Control of a Descent Module during Its Descent in the Earth’s Atmosphere |
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Zubov N., Lapin A., Ryabchenko V.
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Том 61, № 2 (2018) |
Analytical Synthesis of Stabilization Laws for Spacecraft Orbit Attitude Using Information on an Angle and the Full Vector of Angular Velocity |
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Zubov N., Mikrin E., Ryabchenko V., Sorokin I.
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Том 61, № 3 (2018) |
Analyzing and Ensuring the Dynamic Accuracy of the Aircraft Air Data System with a Fixed Flush-Mounted Flow Receiver |
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Soldatkin V., Soldatkin V., Nikitin A., Kornilov V.
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Том 61, № 3 (2018) |
Angle Sensor for a High-Speed Galvo Scanner |
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Gilyazov M., Nagulin K., Gil’mutdinov A.
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Том 60, № 3 (2017) |
Application of a discrete-continuous model of strength analysis to solve the identification problem of a thermally loaded structure |
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Kostin V., Huang S., Valitova N.
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Том 61, № 4 (2018) |
Application of the DRGEP and Engagement Methods to Reduce the Reaction Mechanisms for Calculation of Chemically Non-Equilibrium Flows in Aircraft Engine Nozzles |
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Krioukov V., Abdullin A., Nikandrova M., Safiullin I.
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Том 62, № 4 (2019) |
Application of the Implicit MacCormack Scheme for Computation of Supersonic Turbulent Jets Using the Parabolized Navier—Stokes Equations |
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Molchanov A., Myakochin A., Borovik I., Tushkanov A.
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Том 60, № 1 (2017) |
Application of three-dimensional aerodynamics for calculating trim parameters and flight loads in MSC.Nastran |
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Kvyatkovskaya M., Leont’eva R.
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Том 59, № 2 (2016) |
Approach to implementing hardware-independent automatic control systems of lathes and lathe-milling CNC machines |
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Martinov G., Nezhmetdinov R., Kuliev A.
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Том 62, № 2 (2019) |
Assessment of Improving Performance of an Imitation Model with Respect to the Real Flight Characteristics of a Helicopter |
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Ledyankina O., Girfanov A.
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Том 62, № 4 (2019) |
Assessment of Technical Risks (Reliability) of Aerospace Equipment in the Process of Design and Development |
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Afanas’ev A., Vyashchenko Y., Ivanov K., Matveev S.
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Том 61, № 1 (2018) |
Axial Gas-Dynamic Forces in a Compact Centrifugal Compressor |
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Evgen’ev S., Futin V.
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Нәтижелер 410 - 51/75 |
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