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Searching for optimal configuration of aircraft with annular wings
Lazarev A.Y., Semenov V.N.
Drag function for the striking element sphere-class on subsonic velocity
Romanenko I.V., Crawford K.R., Mitiukov N.W., Busygina E.L.
Drag function for the striking element arrow-class on subsonic velocity
Ganziy Y.V., Salakhov M.M., Mitiukov N.W., Busygina E.L.
Problems and prospect of microgasturbines development for unmanned aerial vehicle propulsion
Zhdanov I.A., Staudacher S., Falaleev S.V.
Method of reducing design aerodynamic characteristics to the results of drain tests of a transport category aircraft model
Bondar Y.I.
The main trends of aviation science development
Alyoshin B.S., Chernyshev S.L.
Methodological support for the training of UAV designers and operators
Lukyanov O.E., Zolotov D.V.
Effect of non-uniform compressor flow parameters on the characteristics of a gas turbine engine combustion chamber
Matveev S.G., Orlov M.Y., Zubrilin I.A., Matveev S.S., Tsybizov Y.I.
Influence of turbulence models on calculated values of aircraft aerodynamic properties
Elisov N.A., Ishkov S.A., Shakhov V.G.
Influence of the turbine ignition, flame tube suspension and nozzles on the combustion chamber characteristics
Matveev S.G., Orlov M.Y., Zubrilin I.A.
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