The disturbed motion of suspend of gyroscope is analysed at cyclic influence of wave of surplus pressure of audio-frequency. The action of flat monochromatic wave and diffuse field is studied. A structure is determined generated by the tense state of suspend of revolting factors resulting in a driftАнализируется возмущенное движение подвеса гироскопа при циклическом воздействии волны избыточного давления звуковой частоты. Изучается действие плоской монохроматической волны и диффузного поля. Определяется структура порождаемых напряженным состоянием подвеса возмущающих факторов, приводящих к дрейфуАналізується збурений рух підвісу гіроскопа при циклічній дії хвилі надлишкового тиску звукової частоти. Вивчається вплив плоскої монохроматичної х...
It is proposed the determination method of power density S for some power functions of time that are...
The one-dimensional electromechanical system with the hauling electric drive of successive excitatio...
The problem of calculation of navigation range and the flight duration, different from estimated tec...
The disturbed motion of suspend of gyroscope is analysed at cyclic influence of wave of surplus pres...
The paper presents the algorithm and the results of the selection of the optimal structure of the fi...
The mathematical model of the wave flow of a non-isothermal liquid film is shown. Wave characteristi...
Experimental data of temperature state and heat transfer characteristics of closed two-phase thermos...
The model of neutralization of the harmful organic impurities containing in ventilating and other ga...
The possibility of using the principles of wet lime treatment technology in semi-reactionary melting...
Parameters of steam-gas phase under cavitation mixing are investigated. According to the following e...
The estimation of a modern condition armour piercing fin stabilized discarding sabot shell for 120 m...
Dependences of influence of constructional peculiarities of shearwalls in frame buildings of LSTC on...
The paper highlights the periods of development of global wind power engineering, characterizes the ...
The article investigates administrative and legal frameworks of activity of Government migratory ser...
In the paper the issues of obtaining the rational structure of statically indeterminate steel concre...
It is proposed the determination method of power density S for some power functions of time that are...
The one-dimensional electromechanical system with the hauling electric drive of successive excitatio...
The problem of calculation of navigation range and the flight duration, different from estimated tec...
The disturbed motion of suspend of gyroscope is analysed at cyclic influence of wave of surplus pres...
The paper presents the algorithm and the results of the selection of the optimal structure of the fi...
The mathematical model of the wave flow of a non-isothermal liquid film is shown. Wave characteristi...
Experimental data of temperature state and heat transfer characteristics of closed two-phase thermos...
The model of neutralization of the harmful organic impurities containing in ventilating and other ga...
The possibility of using the principles of wet lime treatment technology in semi-reactionary melting...
Parameters of steam-gas phase under cavitation mixing are investigated. According to the following e...
The estimation of a modern condition armour piercing fin stabilized discarding sabot shell for 120 m...
Dependences of influence of constructional peculiarities of shearwalls in frame buildings of LSTC on...
The paper highlights the periods of development of global wind power engineering, characterizes the ...
The article investigates administrative and legal frameworks of activity of Government migratory ser...
In the paper the issues of obtaining the rational structure of statically indeterminate steel concre...
It is proposed the determination method of power density S for some power functions of time that are...
The one-dimensional electromechanical system with the hauling electric drive of successive excitatio...
The problem of calculation of navigation range and the flight duration, different from estimated tec...