Constructive actions for decreasing the acoustic pressure inside space-rocket products
Popov P.A., Sindyukov A.A.
Pilot study of frequency characteristics of an acoustic probe for measuring pressure pulsations in the gas turbine engine inlet device
Ivanenko V.N., Alexandrova T.G., Dyagileva E.C., Gimadiyev A.G., Bystrov N.D.
Mathematical model of investigating normal acoustic modes of launch vehicle modules
Popov P.A., Belov A.S., Kryuchkov A.N.
Peculiarities of acoustic loading of the space vehicle in the nose fairing launched as part of a «Soyuz»-type rocket
Popov P.A., Sindyukov A.A., Kryuchkov A.N.
Calculating sound insulation of a sandwich structure on the basis of the «inverse matrix» method
Popov P.A., Osipov A.S., Sindyukov A.A.
Impact of the turbulence modeling approach on the accuracy of the fan noise level prediction
Pyatunin K.R., Arkharova N.V.
Assessment of changes in the sound-proof ability of the rocket fairing with layers of sound-proof materials varying in thickness
Popov P.A.
Development of a small-sized acoustic probe for the measurement of pressure pulsations in the gasdynamic duct of gas turbine engines
Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A.
Application of Bubnov-Galerkin method to determine fixed vibrational loads of launch vehicle compartments
Popov P.A., Sindyukov A.A., Malykhina O.I.
On the development of probes for measuring pressure pulsations in the gas-dynamic channel gas generator
Shorin V.P., Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A., Alexandrova T.G.
Pressure pulsation dampener for air controller
Igolkin A.A., Safin A.I., Shakhmatov E.V.
1 - 11 of 11 Items

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