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Publication : вестник самарского университета

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Academic Journal

Effective use of a station network for information interaction with spacecraft, with a single coordination center

Authors : R. R. Khalilov

Subjects: spacecraft; station network; ground infrastructure management

Source: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol

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Academic Journal

Influence of the characteristics of the working fluids of an electric jet engine on the energy and design parameters of a space vehicle during launch into geostationary orbit

Authors : A. V. Kolesov; V. V. Salmin

Subjects: electric propulsion system; working fluid; xenon

Source: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol

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Academic Journal

Reducing the influence of acoustic vibrations on the operation of flow meters in hydraulic systems of power plants

Authors : F. A. Zaripov; G. I. Pavlov; O. R. Sitnikov

Subjects: pressure pulsations; gas-bubble medium; acoustic energy dissipation

Source: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol

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Academic Journal

Comparative analysis of the energy and finite element methods for determining acoustic loading inside enclosed compartments of aircraft of various configurations

Authors : A. A. Igolkin; P. A. Popov; E. V. Shakhmatov

Subjects: closed objects; energy method; finite element method

Source: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol

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Academic Journal

Validation of the calculation method for determining the soot index using the structural group contribution method for mixtures of petroleum hydrocarbons with biocomponents

Authors : K. D. Tsapenkov; Yu. G. Kuraeva; E. I. Sidorova

Subjects: soot; soot formation indices; fuel

Source: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol

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Academic Journal

Procedure for ensuring the required level of reliability of a propulsion system with a pusher propeller of an aircraft under the influence of foreign objects flying out from under the wheels of the landing gear

Authors : D. S. Markov; E. V. Neskoromny; A. I. Evdokimov

Subjects: pushing propeller; foreign object impact; probability of failure-free operation

Source: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol

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Academic Journal

Assessment of cyclic life of turbine blades in stationary gas turbine units

Authors : A. N. Arkhipov; I. V. Puchkov; Yu. A. Ravikovich

Subjects: turbine blade; elastic-plastic calculation; transient cycle

Source: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol

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Academic Journal

Analytical modeling of circumferential deformation of a hydrodynamical damping device elastic ring with account for friction force

Authors : Ch. Luo; D. K. Novikov; D. S. Diligenskiy

Subjects: amplitude; beam; infinitesimal quantity

Source: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol

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Academic Journal

On-board equipment arrangement taking into account the zones given for on-board cable system routing inside spasecraft compartment

Authors : A. A. Belyakov; A. I. Shulepov; V. М. Papazov

Subjects: on-board equipment; on-board cable system; equipment layout

Source: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol

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Academic Journal

Mathematical model of thermogasdynamic calculation of the actual process in a detonation combustion chamber

Authors : I. M. Gorjunov; Yu. M. Lukin

Subjects: detonation combustion chamber; actual thermodynamic cycle; mathematical model of the detonation combustion chamber

Source: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol

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فلترة النتائج

Effective use of a station network for information interaction with spacecraft, with a single coordination center

Influence of the characteristics of the working fluids of an electric jet engine on the energy and design parameters of a space vehicle during launch into geostationary orbit

Reducing the influence of acoustic vibrations on the operation of flow meters in hydraulic systems of power plants

Comparative analysis of the energy and finite element methods for determining acoustic loading inside enclosed compartments of aircraft of various configurations

Validation of the calculation method for determining the soot index using the structural group contribution method for mixtures of petroleum hydrocarbons with biocomponents

Procedure for ensuring the required level of reliability of a propulsion system with a pusher propeller of an aircraft under the influence of foreign objects flying out from under the wheels of the landing gear

Assessment of cyclic life of turbine blades in stationary gas turbine units

Analytical modeling of circumferential deformation of a hydrodynamical damping device elastic ring with account for friction force

On-board equipment arrangement taking into account the zones given for on-board cable system routing inside spasecraft compartment

Mathematical model of thermogasdynamic calculation of the actual process in a detonation combustion chamber

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