Zobrazeno 1 - 10
of 13
pro vyhledávání: '"L. I. Garipova"'
Publikováno v:
Neftyanoe khozyaystvo - Oil Industry. 7:26-29
Publikováno v:
Neftyanoe khozyaystvo - Oil Industry. 7:40-42
Autor:
George N. Barakos, S.A. Mikhailov, V. Pakhov, A.N. Kusyumov, A.S. Batrakov, L. I. Garipova, Andrey Bozhenko, Robert Stepanov
Publikováno v:
International Journal of Aeroacoustics. 16:460-475
The work documents recent experiments at the Kazan National Research Technical University named after A.N. Tupolev (Kazan Aviation Institute), related to helicopter acoustics. The objective is to measure nar-field acoustics of rotors in hover and pro
Publikováno v:
Russian Aeronautics. 60:198-205
The helicopter main rotor in forward flight is considered in this paper. The results for rigid blades and elastic blades are compared by the method of coupled simulation. The influence of the structural damping coefficient on the blade in-flight defo
Autor:
George N. Barakos, L. I. Garipova, Andrei Sergeevich Batrakov, Sergey Anatolievich Mikhaylov, A.N. Kusyumov
Publikováno v:
International Journal of Numerical Methods for Heat & Fluid Flow. 26:2101-2118
Purpose The design of main rotor blade tips is of interest to helicopter manufactures since the tip details affect the performance and acoustics of the rotor. The paper aims to discuss this issue. Design/methodology/approach In this paper, computatio
Autor:
L. I. Garipova, I. I. Mannanov
Publikováno v:
Oil and Gas Studies. :72-77
Obtaining of the information about reservoir properties of formations is the basis of designing and the results analysis of production stimulation methods. Now two directions have been widely studied and applied, i.e. the hydrodynamic studies impleme
Publikováno v:
Russian Aeronautics (Iz VUZ). 58:419-425
Flows around rotor blade sections equipped with active flaps with a degree of freedom in the flap deflection angle are considered in this paper. Results for oscillating flaps are presented. The resultant flap motion was found to couple with the unste
Publikováno v:
Journal of Aircraft. 52:1634-1643
The aim of this paper is to present aerodynamic analyses of realistic fuselage configurations using computational fluid dynamics. A development model of the Ansat helicopter is employed. The model is tested at the subsonic wind tunnel of the Kazan Na
Autor:
I. I. Mannanov, L. I. Garipova
Publikováno v:
Oil and Gas Studies. :72-76
The authors analyzed the process parameters of the formation acid hydraulic fracturing (FAHF) operations performing taking into account the additional production achieved. The analysis was based on a comparison of results of the laboratory study of t
Publikováno v:
Russian Aeronautics (Iz VUZ). 58:193-198
In this paper, simulation is considered of flow around flapped rotor sections with a degree of freedom in the flap deflection angle. For steady state validation, comparisons one made of numerical results for the flow around a flapped wing with experi