Pesquisa

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Parametric analysis of the anisogrid body of the spacecraft for cleaning the orbit of space debris
Belonovskaya I., Kolga V., Yarkov I., Yarkova E.
Vibration and precision of the details machining
Ramenskaja E., Filippov Y., Latuk D.
Algorithm for simulation of vibration effects during track tests of aircraft and missile technology
Astakhov S., Biryukov V., Borovikov D.
Development of disturbance moments definition method for working reaction flywheels assemblies installed on the special forces measuring stand
Denisova A., Tveryakov O., Britova J.
Determination of the fundamental frequency for rectangular sandwichplate with free edge
Lopatin A., Deev P.
Features of electro-discharge-chemical machining with vibrating electrode-tool
Shestakov I., Remizov I., Artyukova O.
The surface roughness during electro-contact-electrochemical machining with vibration of a cathode-tool
Shestakov I., Semenova L., Shestakov V., Shvaleva N., Remizov I.
MECHANISM OF GENERATING AND DISTRIBUTION OF VIBRATION IN TECHNOLOGICAL MACHINES
Ramenskaya E., Philippov Y., Amelchenko N.
THREE-DIMENTIONAL MODELLING OF EXTERNAL MECHANICAL EFFECTS ON DEVICES AND MACHINERY IN SOLIDWORKS SIMULATION
Martyushev S., Dement’ev A.
Features of achievement of limiting speed values of track tests of ballistic type aircraft
Astakhov S.
ASSESSMENT OF DYNAMIC CHARACTERISTICS OF DESINTEGRATOR WITH ORIGINAL TOOTH GEARING
Schepin A., Kamenetskiy B., Limarenko G., Titov V.
USE OF THE LINEAR ELECTRODYNAMIC ACTUATOR FOR THE RESEARCH OF SHOCK INTERACTION OF MATERIALS
Fadeev A., Shestakov I., Eresko T.
Specific energy consumption of electro-contact-chemical treatment of metals with a vibrating tool in the electrolyte
Shestakov I., Shestakov V., Trifanov I., Remizov I.
THE PROBLEM OF CONSTRUCTION OF MATHEMATICAL MODELS FOR OPTIMIZATION OF PARAMETERS OF FRICTION DAMPERS ON THE EXAMPLE OF BLADES OF GAS TURBINE ENGINES
Rеpetskiy O., Phan V.
INFLUENCE OF REVERBERATION ROOM FORMS ON THE MODAL DENSITY OF THE ACOUSTIC TEST RIG
Lysenko E., Ovchinnikova E.
Characteristics research of a low thrust rocket engine manufactured using additive SLM technology
Akbulatov E., Nazarov V., Gerasimov E.
DEVELOPMENT OF MATHEMATICAL MODELS OF DYNAMICS AND ESTIMATION OF FATIGUE LIFE OF TURBOMACHINES BLADES WITH ACCOUNT OF GEOMETRIC NONLINEARITY
Rеpetskiy O., Bui M.
The shock-absorber for executive powers of system of stabilisation of a spaceCRAFT
Vasiltsov A., Lipovtsev A.
On an alternative method for testing the dynamic strength of a small space-craft structure
Igolkin A., Filipov A.
DETERMINATION OFTHE FUNDAMENTAL FREQUENCY FOR RECTANGULARSANDWICH PLATE WITH TWO FREE EDGES
Lopatin A., Deev P., Lopatin A., Deev P.
Experimental determination of vibration conductivity by rocket sled structural elements in high-speed track tests of aircraft equipment
Astakhov S., Biryukov V., Kataev A.
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