Issue |
Title |
No 1 (2021) |
Effectiveness of 2-D and 3-D modelling of dovetail joint of composite fan blade for choosing rational reinforcement schemes |
|
Guseinov K., Kudryavtsev O.A., Sapozhnikov S.B. |
No 4 (2014) |
Technologies and problems of composite materials mechanics for production of outlet guide vane for aircraft jet engine |
|
Anoshkin A.N., Zuiko V.Y., Shipunov G.S., Tretyakov A.A. |
No 1 (2017) |
Strength computational and experimental analysis of turbojet fan case under the impact of a torn blade |
|
Kurteyev V.A., Burdyugov S.I., Inozemtsev A.A., Lomaev V.I., Mozerov B.G., Sokolovskiy M.I., Shatrov V.B. |
No 3 (2024) |
MULTIPARAMETRIC OPTIMIZATION OF THE ROTOR BLADE DESIGN OF A HELICOPTER WITH CONTROLLED GEOMETRY |
|
Anoshkin A.N., Pisarev P.V., Nureeva E.G., Bayandin S.R. |
No 3 (2023) |
DEVELOPMENT OF A METHOD FOR DESTROYING THE ROTOR BLADES OF A HIGH-PRESSURE COMPRESSOR AT A GIVEN FREQUENTATION OF ROTATION |
|
Gladkiy I.L., Pivovarova M.V. |
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