Zobrazeno 1 - 10
of 44
pro vyhledávání: '"N. P. Adamov"'
Publikováno v:
SIBERIAN JOURNAL OF PHYSICS. 17:34-46
In order to describe the nonlinear behavior of oscillation amplitude of the segmental-conical model on a transversive rod setup in a wind tunnel at Mach М = 2, a polynomial function of damping derivatives was used. Polynom of the 4th degree as a fun
Publikováno v:
Thermophysics and Aeromechanics. 28:1-9
A brief description of measuring means, a free-oscillation setup with a transverse sting of the model, and test conditions is reported. A procedure for processing experimental data is described. Quasi-steady and damping aerodynamic characteristics of
Autor:
E. N. Aleksandrov, E. A. Chasovnikov, A. N. Krylov, N. P. Adamov, A. M. Kharitonov, A. A. Dyad’kin
Publikováno v:
Thermophysics and Aeromechanics. 23:791-800
A setup with free oscillations containing a transverse sting for holding the test model and possible test regimes are described. The method of testing and data processing is presented. Aerodynamic characteristics of the pitching moment of the model i
Publikováno v:
AIP Conference Proceedings.
Aerodynamic derivatives of the pitching moment of a cone mounted on a transverse sting on a setup with free oscillations are obtained. The measurement tools, model, and test regimes are described. The method used to determine the aerodynamic derivati
Autor:
E. A. Chasovnikov, N. P. Adamov
Publikováno v:
AIP Conference Proceedings.
Autor:
M. I. Kazakov, E. A. Chasovnikov, N. P. Adamov, A. N. Krylov, A. M. Kharitonov, A. A. Dyad’kin, A. Yu. Skorovarov
Publikováno v:
Thermophysics and Aeromechanics. 22:535-543
Models of promising reentry vehicles, experimental equipment, and test program are described. The method used to determine the total aerodynamic characteristics of these models on the AB-313 mechanical balance in the T-313 supersonic wind tunnel and
Publikováno v:
Thermophysics and Aeromechanics. 21:679-691
The paper deals with an experimental study of stationary and nonstationary aerodynamic characteristics of a circular cone in the range of Mach numbers 1.75–7. The experimental equipment and the method of determining the aerodynamic characteristics
Autor:
E. A. Chasovnikov, A. M. Kharitonov, A. N. Krylov, A. A. Dyad’kin, L. N. Puzyrev, N. P. Adamov
Publikováno v:
Journal of Applied Mechanics and Technical Physics. 55:870-876
The experimental equipment, model, test conditions, and methods used for determining the streamwise damping on a setup with free oscillations on rolling bearings are described. Characteristics of aerodynamic damping of the model with two positions of
Autor:
E. A. Chasovnikov, L. N. Puzyrev, A. N. Krylov, A. M. Kharitonov, A. A. Dyad’kin, N. P. Adamov
Publikováno v:
Thermophysics and Aeromechanics. 20:729-738
The model, experimental equipment, and test program are briefly described. A method of determining the aerodynamic characteristics of the model on the facility with free oscillations is presented. Aerodynamic derivatives of the pitching moment of the
Autor:
V. I. Zvegintsev, W. Kordulla, M. D. Brodetsky, A. M. Kharitonov, J. Muylaert, L. G. Vasenev, N. P. Adamov, J. C. Paulat, I. I. Mazhul
Publikováno v:
Thermophysics and Aeromechanics. 13:317-326
Results of an experimental study of aerodynamic characteristics of models of two hypersonic re-entry vehicles (ARES-H aerospace demonstrator proposed by EADS-ST and EXPERT re-entry capsule proposed by ESA ESTEC) are presented. The experiments were pe