Contents

Russian Aeronautics

Vol. 65, No. 2, 2022

AIRCRAFT EQUIPMENT

Diagnostics and Forecasting of the Resource of the Alighting Gear Using Artificial Neural Networks

O. S. Dolgov, B. B. Safoklov, and A. A. Smagin p. 225  abstract

Research of Mechanical Impact Effect of the Impactor on the Functional State of Electric Aircraft Li-Ion Batteries

S. A. Savel’ev, I. V. Arbuzov, and D. Yu. Strelets p. 235  abstract

Expert Systems: Means of Information Support for Aircraft Crew Decision Making

N. N. Sukhikh, and V. L. Rukavishnikov p. 243  abstract

STRUCTURAL MECHANICS AND STRENGTH OF FLIGHT VEHICLES

Analysis of Stress Concentration in Locally Loaded Shells

Yu. I. Vinogradov p. 251  abstract

A Technique for Stress-Strain State Analysis, Optimization and Experimental Study of a Hybrid Composite-Metal Propeller Blade

L. P. Shabalin, D. V. Savinov, E. A. Puzyretskii, and I. V. Mareskin p. 260  abstract

FLIGHT DYNAMICS AND CONTROL OF FLIGHT VEHICLES

Synthesis of the Anti-Ship Missile Homing System while Ensuring an Acceptable Oscillation Index of the Stabilization System

Do Quang Thong p. 268  abstract

Preventing the Aircraft from Stalling Along a Sideslip Angle

M. A. Kiselev, S. V. Levitskii, D. V. Moroshkin, and V. A. Podobedov p. 278  abstract

Methods of Coordination and Adaptation of Automatic Control Systems for Gas Turbine Engines with Channel Selectors

V. I. Petunin p. 288  abstract

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

Simulation of Aerodynamic Loads on Structural Elements of Landing Platform whilst Helicopter Takeoff and Landing

K. N. Volkov, V. N. Emel’yanov, M. S. Yakovchuk, and N. S. Khar’kov p. 297  abstract

Research of an Aerodynamically Short Nozzle Ring with Embedded Load-Carrying Airfoils

V. V. Vyatkov, A. M. Toshchakov, and L. A. Remizov p. 306  abstract

Calculation of the Loads behind the Triple Configuration of Partially Localized Shock Waves on the Aircraft Structural Elements

A. S. Kapralova p. 311  abstract

Triple Configurations of Steady and Propagating Shocks

M. V. Chernyshov, and L. G. Gvozdeva p. 319  abstract

AIRCRAFT AND ROCKET ENGINE DESIGN AND DEVELOPMENT

Development of Methods for Designing Turbines and Compressors as a Part of Gas Turbine Engines

I. A. Krivosheev, K. E. Rozhkov, and N. B. Simonov p. 345  abstract

AIRCRAFT AND ROCKET ENGINE THEORY

Estimation of a Range of Possible Parameters for a Hybrid Turbine Engine with Solid Oxide Fuel Cells for Airliner

A. B. Agul’nik, S. M. Kalenskii, I. V. Kravchenko, and Yu. A. Ezrokhi p. 361  abstract

The Effect of Flight Overload on the Intra-Chamber Process in a Solid-Propellant Rocket Engine

M. Yu. Egorov p. 368  abstract

Enhancement of Wall Cooling by Single-Cavity Diffuser-Type Dimples in Turbulent Flow

A. V. Il’inkov, A. V. Shchukin, V. V. Takmovtsev, I. Sh. Zaripov, and I. I. Khabibullin p. 380  abstract

AIRCRAFT PRODUCTION TECHNOLOGY

Influence of Vibrations on the Accuracy of Measurement by Using Laser Coordinate Measuring Systems in Production Conditions

P. L. Lyudogovskii, V. L. Fedyaev, and M. A. Komkova p. 386  abstract

Comparative Modeling of Hybrid Intelligent Control System for Aviation Production

A. M. Pishchukhin, and G. F. Akhmed’yanova p. 393  abstract

RADIO ENGINEERING AND COMMUNICATION

Analysis of the Possibility of Detecting the Wires of High-Voltage Overhead Power Transmission Lines to Ensure the Aircraft Flight Safety

B. K. Sivyakov, A. A. Skripkin, and D. B. Sivyakov p. 400  abstract

Algorithm for Detecting the Critical Elements of Airborne Radar Systems Based on Operational Analysis of Diagnostic Information Time Series

V. A. Shevtsov, A. V. Timoshenko, A. Yu. Perlov, and K. V. L’vov p. 405  abstract

AIRCRAFT EQUIPMENT

Electric Multicopter Battery Selection and Hovering Power

S. Z. Sverdlov p. 413  abstract

Human-Autonomy Teaming Interface Design for Multiple-UAV Control

A. M. Fedulin, D. V. Evstaf’ev, G. L. Kondrashova, and N. V. Artemenko p. 419  abstract

FLIGHT DYNAMICS AND CONTROL OF FLIGHT VEHICLES

Algorithmic Method for Improving the Fault Tolerance of the Automatic Control and Monitoring System of a Turbojet Bypass Engine

A. A. Inozemtsev, N. G. Lamanova, A. N. Sazhenkov, I. N. Gribkov, and A. S. Pleshivykh p. 425  abstract

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

Exact Solutions of the Navier–Stokes Equations for Describing the Rotating Fluid

O. A. Ledyankina, E. Yu. Prosviryakov, and E. V. Romanova p. 431  abstract