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Types of aeroelastic vibrations of turbomachinery bladed discs
Koskin A.O., Seleznev V.G.
Calculation of exciting aerodynamic load on a gas turbine engine compressor blade induced by the effect of a non-uniform gas flow
Ermakov A.I., Shklovets A.O., Fedorchenko D.G.
Verification of a design model and evaluation of a technique of manufacturing aircraft engine composite parts on the basis of dynamic tests
Zinin A.V., Arkhipov A.N., Kholobtsev D.P., Ravikovich Y.A., Shevjakov A.O., Kholmanova M.A.
Parameters transducers of the blade’s dynamic movements of turbounits based on nonlinear approximation of primary signals
Chernyavskiy A.Z., Danilin A.I., Danilin S.A.
About relaxational resistance of the compressor’s blades from titanium alloys
Smyslov A.M., Smyslova M.K., Dubin A.I.
The device for the determination of blades oscillation parameters based on nonlinear approximation of primary transducers signals
Danilin A.I., Chernyavskiy A.Z., Danilin S.A.
Development of magnetic fluid dampers of aicrafts chassis elements
Averianov G.S., Belkov V.N., Korchagin A.B., Agarin M.Y.
Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor
Posadov V.V., Remizov A.E.
Method of pipeline system designing taking into account complex interaction of static and dynamic processes with strength characteristics
Mironova T.B., Prokofiev A.B., Rodionov L.V.
Resonant converter with PWM output voltage adjustment
Vorokh D.A., Makhov A.I.
Van der Pol, Rayleigh and Duffing oscillators in discrete time dynamics
Zaitsev V.V., Nuraev D.B., Shilin A.N.
Calculation of the performance of a coulomb friction damper of a crown bevel gear wheel for different forms of resonant oscillations
Kozharinov E.V., Temis J.M.
1 - 12 of 12 Items

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