Zobrazeno 1 - 7
of 7
pro vyhledávání: '"B. A. Smolnikov"'
Autor:
A. S. Smirnov, B. A. Smolnikov
Publikováno v:
Vestnik St. Petersburg University, Mathematics. 56:93-106
Autor:
A. S. Smirnov, B. A. Smolnikov
Publikováno v:
Vestnik St. Petersburg University, Mathematics. 55:243-248
Autor:
B A Smolnikov, A S Smirnov
Publikováno v:
Journal of Physics: Conference Series. 1959:012046
The article studies nonlinear oscillations of a double mathematical pendulum which axes of the cylindrical joints are not collinear to each other and constitute an acute angle between themselves. Nonlinear oscillation modes of the system are construc
Autor:
A S Smirnov, B A Smolnikov
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 1129:012042
The article investigates nonlinear oscillations of the double mathematical pendulum having identical parameters of its links and end loads. Approximate solutions in the nonlinear zone are constructed and analyzed on the basis of exact solution in the
Autor:
B. A. Smolnikov, Alexander K. Belyaev
Publikováno v:
Acta Mechanica. 195:365-377
The paper deals with the comparative analysis of stability of the torque-free rotation of a rigid body and a solid with internal dissipation. It is shown that the dissipation-induced instability has a critical influence on stability of the rotating b
Autor:
V. A. Leontiev, B. A. Smolnikov
Publikováno v:
Cosmic Research. 42:382-388
The problems of investigation and optimization of the motion of spacecraft are extensively discussed in the literature. Nevertheless, in many cases a large variety of qualitative characteristics of their motion and of the form of their trajectories a
Autor:
Andrey V. Korshunov, V. O. Sabadash, B. A. Smolnikov, Evgenij N. Pyatishev, Mihail S. Lurie, Y. D. Akulshin, Alexei I. Borovkov
Publikováno v:
Fourth International Workshop on Nondestructive Testing and Computer Simulations in Science and Engineering.
Measurements of acoustic pressure oscillations on curvilinear surface streamlined by a flow, for example, on the wall of wind-tunnel or airfoil is necessary to supply for aeroacoustic appendices. Microphone should have the minimal sizes and feeler se