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Vol 16, No 1 (2017)

Types of aeroelastic vibrations of turbomachinery bladed discs

Koskin A.O., Seleznev V.G.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

About relaxational resistance of the compressor’s blades from titanium alloys

Smyslov A.M., Smyslova M.K., Dubin A.I.

(Rus)

Vol 11, No 5-2 (2012): Special Issue

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.

(Rus)

Vol 11, No 5-2 (2012): Special Issue

Development of magnetic fluid dampers of aicrafts chassis elements

Averianov G.S., Belkov V.N., Korchagin A.B., Agarin M.Y.

(Rus)

Vol 15, No 4 (2016)

Method of vibration diagnostics of aerodynamic and aeroelastic oscillations in gas turbine engine compressor

Posadov V.V., Remizov A.E.

(Rus)

Vol 12, No 2 (2013)

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.

(Rus)

Vol 15, No 3 (2016)

Resonant converter with PWM output voltage adjustment

Vorokh D.A., Makhov A.I.

(Rus)

Vol 15, No 1 (2016)

Van der Pol, Rayleigh and Duffing oscillators in discrete time dynamics

Zaitsev V.V., Nuraev D.B., Shilin A.N.

(Rus)

Vol 14, No 3-1 (2015): Special Issue

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.

(Rus)

Vol 13, No 5-4 (2014): Special Issue

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.

(Rus)

Vol 18, No 4 (2019)

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.

(Rus)

Vol 11, No 7 (2012)

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.

(Rus)

1 - 12 of 12 Items

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