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Title
Authors
An Anthropocentric Approach for Solving the Problem of Optimal Automatic Landing Flare
Trinh V.T., Nguyen N.M., Dang N.T., Nguyen K.A.
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.
Thermally excited vibrations of aircraft structural elements
Starovoitov E.I., Leonenko D.V., Rabinskii L.N.
Identification Method of the Time-Series Properties of the Aviation Events
Zenchenko T.A., Gorshkov V.A., Sirotin N.N., Frolkov A.I., Pleshakov A.I.
Study of Procedure Errors of the Vortex Air Data System of a Subsonic Aircraft
Efremova E.S., Soldatkin V.V.
The Stressed State of a Stiffened Conical Shell with Thermal Protective Coating with Temperature-Dependent Properties
Bakulin V.N., Vinogradov Y.I., Men’kov G.B.
Problems and prospects of using gas and hydrodynamic lubricants in support seals of aircraft engine rotors
Balyakin V.B.
Electric charge imposition on hydrocarbon fuel drops in sharply inhomogeneous electric field of injector modules
Kolodyazhnyi D.Y., Nagornyi V.S.
Ways to Manage Small-Scale Machine-Building Production
Ivanov V.K.
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.
Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System
Kornev A.V., Sereda V.A., Migalin K.V.
Influence of combustion chamber geometry and compression ratio on the main parameters of a diesel aircraft engine
Gureev V.M., Khairullin A.K., Varlamov F.A., Gumerov I.F., Khafizov R.K.
A simulator of the aircraft air data system
Efremova E.S.
Design Features and Efficiency Analysis of the Aircraft Complex Air Data System with a Fixed Flush-Mounted Flow Receiver
Soldatkin V.M.
Analyzing and Ensuring the Dynamic Accuracy of the Aircraft Air Data System with a Fixed Flush-Mounted Flow Receiver
Soldatkin V.M., Soldatkin V.V., Nikitin A.V., Kornilov V.Y.
Design and Experimental Analysis of Aircrew Design Parameters to Vertical Takeoff and Landing
Gainutdinova T.Y., Gainutdinov V.G.
On similarity criteria in flight mechanics
Golovkin M.A., Deryabin E.Y.
Experimental investigation of lift for a wing-in-ground effect aircraft model
Nazarov D.V., Frolov V.A., Shakhov V.G.
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