Vol. 66, No. 2, 2023

Russian Aeronautics

AIRCRAFT EQUIPMENT

Computational Method for Evaluation of a Disk-Type Electrical Machine with Permanent Magnets

F. R. Ismagilov, V. E. Vavilov, I. F. Sayakhov, and E. A. Pronin p. 195 abstract

STRUCTURAL MECHANICS AND STRENGTH OF FLIGHT VEHICLES

Influence of Dimensions of Rectangular Cutouts and Modulus of Elasticity of Reinforcing Embedded Elements on the Stress-Strain State of Sandwich Compartments

V. N. Bakulin p. 204 abstract

Energy Concept of the Surface of Metal Aircraft Parts

V. S. Oleshko p. 216 abstract

AERO- AND GAS-DYNAMICS OF FLIGHT VEHICLES AND THEIR ENGINES

Mathematical Modeling of Operation of the Electrically Driven Propeller

B. L. Artamonov, and V. O. Lukhanin p. 223 abstract

Outflow of Supersonic Gas Jets from Axisymmetric Nozzle into a Space with a High Nozzle Pressure Ratios

D. O. Bogdaniuk, K. N. Volkov, V. N. Emel’yanov, and A. V. Pustovalov p. 232 abstract

Research of Ducted Propellers. Comparison of Ducted Propellers with Conventional Single-Row and X-Shaped Double-Row Propellers

M. P. Bulat, L. O. Vokin, and I. A. Volobuev p. 242 abstract

Inter-Caliber Sector-Type Air Intake Device

V. V. Vetrov, A. A. Vorob’ev, and P. D. Shilin p. 247 abstract

On Optimum Coolant Injection into a Laminar Boundary Layer in Supersonic Gas Flows

K. G. Garaev, T. K. Garaev, and D. M. Osadchaya p. 252 abstract

Research of Ducted Propellers. Comparison of Coaxial, Four Bladed, and Eight-Bladed Counter-Rotating Propeller

S. Yu. Dudnikov, P. N. Kuznetsov, and A. I. Mel’nikova p. 259 abstract

Analysis of Effectiveness of the External Expansion Nozzle with a Perforated Central Body

Yu. V. Kaun, and M. V. Chernyshov p. 267 abstract

Spectral Characteristics of Three-Dimensional Flow around a Circular Cylinder

S. A. Kusyumov, A. N. Kusyumov, and E. V. Romanova p. 276 abstract

Nonequilibrium Homogeneous Condensation in Supersonic Multiphase Flows

A. M. Molchanov, and M. V. Siluyanova p. 283 abstract

AIRCRAFT AND ROCKET ENGINE THEORY

Specific Features of Transient Processes in Stationary Plasma Thrusters and a Device for Their Simulation

R. V. Akhmetzhanov, A. V. Bogatyi, V. Kim, E. V. Rudenko, and E. A. Shilov p. 293 abstract

Film Cooling Forming Features of the Turbine Nozzle Vanes Leading Edge Neighborhood Taking into Account Entry Flow Irregularity

V. V. Vyatkov, A. A. Davydov, N. N. Kovaleva, and A. M. Toshchakov p. 308 abstract

Conjugate Heat Transfer Validation of Gas Turbine Engine Cooling Turbine Vanes

Yu. G. Gorelov p. 316 abstract

Heat Transfer in Diffuser-Type Dimples Streamlined by Pulsating Flow

A. V. Il’inkov, V. V. Takmovtsev, A. V. Starodumov, A. V. Shchukin, and R. A. Vasin p. 325 abstract

Influence of Incidence on Streamlines and Profile Losses of Turbine Cascades

B. I. Mamaev, and G. V. Ermolaev p. 332 abstract

AIRCRAFT INSTRUMENTS AND INSTRUMENTATION COMPUTER COMPLEXES

Tools for Researching Some Aspects of Reliability and Service Life of Semiconductor Spark Plugs

F. A. Gizatullin, and O. A. Yushkova p. 343 abstract

AIRCRAFT PRODUCTION TECHNOLOGY

Tacit Knowledge Service on Industrial Robot Selection for Efficient Aircraft Production Based on the Flexible MADM Approach

Md Helal Miah, Jianhua Zhang, and Gurmail Singh Malhi p. 349 abstract

AUTOMATION OF DESIGN AND PRODUCTION OF AERONAUTICAL EQUIPMENT

A Technique of Hydraulic System Optimization at the Preliminary Design Stage by the NSGA-II Genetic Algorithm

I. O. Bobarika, and A. S. Gruzdev p. 387 abstract

RADIO ENGINEERING AND COMMUNICATION

Calculation of Reliability Parameters of Onboard Harness with Aluminum Wires

I. S. Vasil’ev, S. V. Efremov, A. P. Leonov, and S. B. Suntsov p. 396 abstract

Modernization of the Shape Control System for the Radio-Reflecting Surface of a Transformable Space Antenna

Yu. V. Konoplev, A. D. Shirshov, and A. A. Yuev p. 404 abstract

FLIGHT DYNAMICS AND CONTROL OF FLIGHT VEHICLES

The Concept of a Force-Measuring Device for Ground Testing of Propulsion System Demonstrators

A. R. Vorob’ev, E. A. Mikhailov, and V. B. Fedorov p. 409 abstract

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