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Control of a Piezo Actuator to Adjust the Reflective Surface of the Space-Based Reflector
Kabanov S.A., Mitin F.V., Krivushov A.I., Ulybushev E.A.
Research on High-Precision Measurement Systems of Modern Aircraft
Shen K., Neusypin K.A., Selezneva M.S., Proletarskii A.V.
Computation of design parameters influence on air injector fuel atomization
Sipatov A.M., Modorskii V.Y., Babushkina A.V., Kolodyazhnyi D.Y., Nagornyi V.S.
Estimation of mode onset for reverse jet reattachment to the engine nacelle in a flow
Varsegov V.L.
Simulation of thermal radiation emitted by heterogeneous combustion products in the combustion chamber of a model engine
Kuz’min V.A., Maratkanova E.I., Zagrai I.A., Rukavishnikova R.V.
A Method of Calculating the Small-Sized Combustion Chambers
Lanskii A.M., Lukachev S.V., Matveev S.G., Kolomzarov O.V.
Numerical Determination of Contact Forces in Radial Roller Bearings with Flexible Rings
Ivannikov V.V., Degtyarev S.A., Popov V.V., Sorokin F.D., Leont’ev M.K.
A Quasi-Spherical Air Pressure Probe
Golovkin M.A., Efremov A.A., Sysoev V.V.
Physical modeling of electromagnetic interferences in the unmanned aerial vehicle in the case of high-voltage transmission line impact
Nuriev M.G., Gizatullin Z.M., Gizatullin R.M.
A mathematical model of transforming the vertical takeoff and landing aircraft with a disk wing at maneuvering (on a deck)
Pavlov V.V.
Studies of GTE reverse jets distribution
Mingaleev G.F., Margulis S.G., Kosterin A.V.
Deformation of the Shell of the Cylindrical Cryogenic Tank during its Filling
Zarubin V.S., Zimin V.N., Kuvyrkin G.N.
Effect of a Model and Boundary Conditions on the Results of Analyzing the Stress-Strain State of a Low-Pressure Compressor Rotor
Arkhipov A.N., Volgina M.V., Matushkin A.A., Ravikovich Y.A., Kholobtsev D.P.
An Anthropocentric Approach for Solving the Problem of Optimal Automatic Landing Flare
Trinh V.T., Nguyen N.M., Dang N.T., Nguyen K.A.
Numerical determination of the gas-dynamic behavior of vane cascades with various deflection angles of the trailing edges of longitudinal ribs of an advanced gas-turbine engine thrust reverser
Varsegov V.L., Shabalin A.S.
Composite model of a research flight simulator for a helicopter with the hingeless main rotor
Ledyankina O.A., Mikhailov S.A.
Computational modeling of interference between helicopter main and tail rotors based on nonlinear blade vortex model
Ignatkin Y.M., Makeev P.V., Shomov A.I.
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