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