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An Anthropocentric Approach for Solving the Problem of Optimal Automatic Landing Flare
Trinh V.T., Nguyen N.M., Dang N.T., Nguyen K.A.
Principles of Constructing the Systems of Restriction the Aircraft Critical Parameters
Petunin V.I., Neugodnikova L.M.
Influence Analysis of the Second Bypass Air Bleed Parameters on the Engine Performance
Agul’nik A.B., Kravchenko I.V., Gorbunov A.A., Novoselova A.A., Sklyarova A.P.
On the Problem of Improving the Flight Safety in Manual Control of the Aircraft
Garkushenko V.I., Lazareva P.A.
Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution
Zubov N.E., Mikrin E.A., Ryabchenko V.N., Fomichev A.V.
Technique of physical modeling of lightning strike effects on aircraft
Gizatullin Z.M., Gizatullin R.M., Nuriev M.G.
Risk of Passenger Injuries in the Virtual Certification Tests of an Aircraft Seat Unit
Shabalin L.P., Sidorov I.N., Gorelov A.V.
Synthesis of Stabilization Laws for Lateral Motion of a Maneuverable Aircraft at the Lack of Data on Its Sideslip and Roll Angles
Zubov N.E., Mikrin E.A., Ryabchenko V.N., Sorokin I.V.
Research on High-Precision Measurement Systems of Modern Aircraft
Shen K., Neusypin K.A., Selezneva M.S., Proletarskii A.V.
Analysis of Errors for Measuring Channels of Aircraft Air Data System with a Fixed Non-Protruding Flow Receiver
Krylov D.L., Soldatkin V.M., Efremova E.S.
Influence of exhaust gas recirculation on technical, economic, and environmental performance of high-uprated diesel aircraft engine
Gureev V.M., Khairullin A.K., Varlamov F.A., Gumerov I.F., Khafizov R.K.
Studies of GTE reverse jets distribution
Mingaleev G.F., Margulis S.G., Kosterin A.V.
Impact Analysis of Sharp Cone Shape Small Changes on the Position of its Pressure Center at Supersonic and Hypersonic Flow with a Small Angle of Attack
Mokin Y.A., Kiselev V.I., Meshchanov A.S.
Integration of a High-Pressure Gas Turbine of the Gas Turbine Engine with a Gas-Dynamic Laser
Perel’shtein B.K., Osipov B.M., Titov A.V.
Continuous Flight Safety Management Information System for a Group of Converging Aircraft
Goncharenko V.I., Lebedev G.N., Mikhailin D.A., Khakhulin G.F.
Study of performance of the aircraft gas turbine engine integrated with a gas dynamic laser
Osipov B.M., Kopelevich L.A., Perel’shtein B.K.
Improvement of handling qualities for the aircraft longitudinal motion
Garkushenko V.I., Vinogradov S.S.
A Wheel Motor for Aircraft Application
Afanas’ev A.Y., Karimov A.R., Studneva E.E.
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.
Methodological foundations and areas for improvement of the aircraft design process
Liseitsev N.K., Matveenko A.M., Ovcharenko V.N.
Route optimization of the aircraft flight
Averkiev N.F., Vlasov S.A., Salov V.V., Kiselev V.V.
Hyperbolic Paraboloid for a Ruled Preform of an X-Fitting: Calculation of Parameters
Khaliulin V.I., Savitskii V.V., Zhukov A.V., Gimadiev R.S.
Problem of the Community Noise Reduction for Aircraft with Open Rotor Engines
Moshkov P.A., Samokhin V.F., Yakovlev A.A.
Numerical Simulation of Detachment Dynamics of a Payload from the Parent Aircraft
Bykov L.V., Pashkov O.A., Pravidlo M.N., Tishkov V.V., Yanyshev D.S.
Layout of the power plant with an odd number of engines on the wing of the middle-range passenger aircraft
Gusev V.G.
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