Zobrazeno 1 - 10
of 52
pro vyhledávání: '"I. S. Tsyryulnikov"'
Publikováno v:
Thermophysics and Aeromechanics. 29:659-672
Autor:
S. V. Kirilovskiy, T. V. Poplavskaya, S. G. Mironov, I. S. Tsyryulnikov, I. R. Valiullin, T. S. Militsina
Publikováno v:
Thermophysics and Aeromechanics. 29:703-714
Publikováno v:
SIBERIAN JOURNAL OF PHYSICS. 17:22-28
Methods for restoring aerodynamic forces based on the use of measurement data by balance elements and an accelerometer have been expanded. A signal processing method has been developed that makes it possible to correct the measurement data of balance
Autor:
T. V. Poplavskaya, I. R. Valiullin, S. V. Kirilovskiy, T. S. Militsina, S. G. Mironov, I. S. Tsyryulnikov
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Autor:
I. R. Valiullin, S. V. Kirilovskiy, T. S. Militsina, S. G. Mironov, T. V. Poplavskaya, I. S. Tsyryulnikov
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Publikováno v:
Thermophysics and Aeromechanics. 28:821-825
Publikováno v:
Journal of Applied Mechanics and Technical Physics. 62:183-192
Results of experimental and numerical investigations of a supersonic flow of cylindrical models aligned at a zero angle of attack with frontal inserts made of cellular porous nickel are reported. The experiments are performed in a supersonic wind tun
Autor:
T. V. Poplavskaya, I. S. Tsyryulnikov
Publikováno v:
Thermophysics and Aeromechanics. 28:29-39
Relations for the coefficients of transformation of disturbances to pressure oscillations for the case of long-wave disturbances of the external flow are derived from the general analytical solution of the inviscid problem of disturbance interaction
Publikováno v:
Journal of Applied Mechanics and Technical Physics. 61:693-699
Results of experimental and numerical modeling of a supersonic flow around a cylinder with a frontal gas-permeable high-porosity insert aligned at different angles of attack are presented. The experiments are performed in a supersonic wind tunnel at