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Automation of conceptual design and modification of aircraft type unmanned aerial vehicles using multidisciplinary optimization and evolutionary algorithms. Part 1: Methods and models
Komarov V.A., Lukyanov O.E., Hoang V.H., Kurkin E.I., QuijadaPioquinto J.G.
Drag function for the striking element sphere-class on subsonic velocity
Romanenko I.V., Crawford K.R., 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.
The main trends of aviation science development
Alyoshin B.S., Chernyshev S.L.
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 the turbine ignition, flame tube suspension and nozzles on the combustion chamber characteristics
Matveev S.G., Orlov M.Y., Zubrilin I.A.
Methodological support for the training of UAV designers and operators
Lukyanov O.E., Zolotov D.V.
Influence of turbulence models on calculated values of aircraft aerodynamic properties
Elisov N.A., Ishkov S.A., Shakhov V.G.
Searching for optimal configuration of aircraft with annular wings
Lazarev A.Y., Semenov V.N.
1 - 9 of 9 Items

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