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Title
Authors
Vol 17, No 1 (2016)
EVALUATION OF THE INFLUENCE OF DIAMETER PROPELLER ON THE ACOUSTICS CHARACTERISTIC OF THE POWER PLANT BY THE LIGHT AIRCRAFT
Moshkov P.A., Samokhin V.F.
Vol 26, No 2 (2025)
Overview of unmanned aircraft cargo delivery systems
Solomin E.V., Martyanov A.S., Shahin H., Pshenisnov N.A., Sheryazov S.K.
PDF
(Rus) PDF
(Eng)
Vol 24, No 2 (2023)
The use of cylindrical wing propellers in aviation technology
Prokhorov V.V., Oborin L.A., Melnikov V.P.
PDF
(Rus)
Vol 19, No 2 (2018)
DEVELOPMENT OF THREE-POINT AVIATION FUEL QUANTITY GAUGE
Akzigitov R.A., Statsenko N.I., Pisarev N.S., Efimova A.N.
PDF
(Rus)
Vol 24, No 1 (2023)
The aircraft hydraulic system units and pipelines heat exchange parameters study
Nikolaev V.N.
PDF
(Rus)
Vol 19, No 4 (2018)
METHOD OF QUALITY ANOMALIES DETECTION IN INTERACTIVE ELECTRONIC TECHNICAL MANUALS FOR AIRCRAFT MAINTENANCE AND REPAIR
Frolova E.A., Ivakin Y.A., Smirnov A.O.
PDF
(Rus)
Vol 10, No 3 (2009)
Preliminaries to chooisingan automated control system structure of aircrafts
Kovalev I.V., Nurgaleeva J.A., Gritsenko S.N., Usachev A.V.
PDF
(Rus)
Vol 18, No 1 (2017)
STATISTICAL ANALYSIS OF THE RELATIONSHIP OF CONSTRUCTIVE CHARACTERISTICS OF AIRCRAFTS
Balaban E.I., Bunakov P.Y., Gal’chenko A.V., Tegin V.A.
PDF
(Rus)
Vol 13, No 3 (2012)
THEORETICAL JUSTIFICATION OF ALGORITHM OF DETERMINATION OF AIRCRAFT ROTATING MASS MOMENTS
Ushakov N.U.
PDF
(Rus)
Vol 17, No 2 (2016)
APPLICATION OF SENSITIVE FUNCTIONS, WHICH USED TO COMPUTE TUBES INCLUDING THE TRAJECTORIES OF CONTROL SYSTEMS
Rogalyov A.N.
Vol 12, No 4 (2011)
SOLUTION OF A PROBLEM OF SUPPORT OF THE DESISION TO BE MADE BY A CREW TEAM WHEN AN EMERGENCY SITUATION OCCURS WILE IN FLIGHT
Lukasov V.V., Nikushkin N.V.
PDF
(Rus)
Vol 16, No 3 (2015)
MANUFACTURING TECHNOLOGY AND WELDING OF ALUMINUM ALLOYS ELECTRODES CONTAINING NANOPOWDERS
Krushenko G.G.
Vol 25, No 4 (2024)
Algorithm for correcting camera pan and tilt on aircraft based on recorded video
Nikiforov D.L., Efimov S.N.
PDF
(Rus) PDF
(Eng)
Vol 16, No 1 (2015)
NUMERICAL ESTIMATIONS OF MAXIMUM DEVIATIONS FOR AIRCRAFT TRAJECTORIES IN THE ATMOSPHERE
Rogalyov A.N., Rogalyov A.A.
PDF
(Rus)
Vol 24, No 3 (2023)
Tool material selection methodology for aircraft elements design
Faizullin K.V., Danilaev M.P., Polyaev A.V., Semin N.A., Rakipov T.I.
PDF
(Rus) PDF
(Eng)
Vol 14, No 2 (2013)
INVESTIGATION OF FLOW-AROUND THE HEMISPHERICAL WING IN A GAS OUTERMOST FLOW
Proteven I.S., Kraev M.V.
PDF
(Rus)
Vol 21, No 1 (2020)
Analysis of the ADS-B airspace monitoring system
Akzigitov A.R., Akzigitov R.A., Ogorodnikova Y.V., Dmitriev D.V., Andronov A.S.
PDF
(Eng)
Vol 19, No 3 (2018)
APPLICATION OF THE BOOTSTRAP METHOD FOR STATISTICAL CHARACTERISTICS ASSESSMENT OF AIRCRAFT COMPONENTS’ SMALL SAMPLES
Gerasimova D.S., Sayapin A.V., Palukhin A.A., Katsura A.V.
PDF
(Rus)
1 - 18 of 18 Items

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