Contents

Russian Aeronautics

Vol. 65, No. 4, 2022

AIRCRAFT EQUIPMENT

The Impact of Fuel Fluidity in Wing Tanks on the Aeroelasticity Characteristics of an Aircraft

S. F. Borodkin, M. A. Kiselev, V. V. Ovchinnikov, and Yu. V. Petrov p. 629  abstract

Issues of Ensuring the Vibration Resistance for Modern Aircraft Electronics Units

F. R. Ismagilov, V. E. Vavilov, I. I. Yamalov, R. R. Urazbakhtin, and A. I. Bikchurin p. 639  abstract

Design, Development and Testing of a Starter-Generator Based on a Brushless DC Electric Machine for an APD-500 Aircraft Piston Engine Demonstrator

L. A. Finkel’berg, V. E. Vavilov, D. R. Farrakhov, A. N. Kostyuchenkov, and I. F. Sayakhov p. 646  abstract

FLIGHT VEHICLE DESIGN

Application of Perforated Stabilizers for Static Stability at Subsonic Flight Speeds of the Separation Unit of a Spacecraft Emergency Escape System

V. T. Kalugin, A. Yu. Lutsenko, M. D. Kalugina, D. K. Nazarova, and D. M. Slobodyanyuk p. 655  abstract

Computational Assessment of the Efficiency of Using Various Fuel Pairs Onboard a Small Spacecraft

A. A. Levikhin, and A. I. Musteikis p. 662  abstract

STRUCTURAL MECHANICS AND STRENGTH OF FLIGHT VEHICLES

Layer-by-Layer Study of the Stress and Strain State of Sandwich Conical Aircraft Compartments with Rectangular Cutouts

V. N. Bakulin p. 668  abstract

Nonlinear Deformation and Stability of a Composite Cylindrical Shell under Combined Loading by Torsion and Bending Moments

I. P. Zheleznov p. 677  abstract

FLIGHT DYNAMICS AND CONTROL OF FLIGHT VEHICLES

Simulation of Exoskeleton Motion during a Flight on a Movable Base Taking into Consideration the Electric Drive Dynamics

V. K. Badyaeva, A. O. Blinov, A. V. Borisov, and R. G. Mukharlyamov p. 685  abstract

An Algorithm of Aircraft Attitude and Distance Estimation Relative to the Landing Platform with Optical Marks

T. Yu. Gainutdinova, A. I. Badekha, A. V. Gainutdinova, and V. G. Gainutdinov p. 697  abstract

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

Investigation of Gas Flow Characteristics When Using Intra-Nozzle Interceptors to Control the Thrust Vector

N. A. Brykov, and K. O. Tishchenko p. 705  abstract

Comparison of Turbulence Models in the Numerical Simulation of the Model Ducted Propeller

P. V. Bulat, N. V. Prodan, and L. O. Vokin p. 713  abstract

Parametric Analysis of Air Intake Design Schemes and Its Impact on Aerodynamic Layout

V. V. Vetrov, V. V. Morozov, and P. D. Shilin p. 722  abstract

Gas-Particle Flow around an Expansion Corner

K. N. Volkov, and V. N. Emel’yanov p. 731  abstract

Numerical Simulation of Flow over Elliptical Airfoils with Different Curvature

S. A. Kusyumov, A. N. Kusyumov, and S. A. Mikhailov p. 741  abstract

Investigation of Lifting Properties of the Fuselage Constructed by Airfoils with Air Extraction at the Upper Critical Point for a Short Take-Off and Landing Air Taxi

A. I. Mel’nikova, P. N. Kuznetsov, and M. P. Bulat p. 749  abstract

AIRCRAFT AND ROCKET ENGINE DESIGN AND DEVELOPMENT

Mathematical Modeling of Loading for Remanufactured Compressor Blades of Gas Turbine Engines

O. A. Bytsenko, D. S. Martynkevich, V. S. Oleshko, and N. O. Strizhevskaya p. 758  abstract

Noise Suppression in Aircraft Nozzle Calibration Facilities

O. A. Dushina, A. A. Valeev, N. S. Dushin, and S. A. Kolchin p. 764  abstract

Dynamics of Roller Bearings of Gas Turbine Engines under Hydrodynamic Friction

Ya. M. Klebanov, V. V. Murashkin, A. I. Danil’chenko, V. R. Petrov, and K. A. Polyakov p. 772  abstract

AIRCRAFT AND ROCKET ENGINE THEORY

The Method for Optimization of a Countercurrent Recuperative Heat Exchanger for a Cryogenic System Used in Superconducting Transport Power Plants

Yu. I. Ermilov, Yu. A. Ravikovich, and D. P. Kholobtsev p. 779  abstract

Efficiency of Heat Shield Generated by Blowing the Pulsating Airflow through One-Row Bands of Holes

A. V. Il’inkov, V. V. Takmovtsev, A. L. Tukmakov, A. V. Shchukin, and I. S. Baranov p. 791  abstract

Numerical Study of Viscous Flows in Rocket Engine Nozzles with an Optimized Supersonic Part and Separation of the Laminar Boundary Layer from the Wall

I. A. Kryukov, I. E. Ivanov, and S. A. Shustov p. 799  abstract

AIRCRAFT INSTRUMENTS AND INSTRUMENTATION COMPUTER COMPLEXES

Method for Equipping the Aircraft Gas Turbine Engine with Vibration Sensors by Evaluating Their Information Content Based on Mathematical Modeling

K. V. Shaposhnikov, A. V. Davydov, S. A. Degtyarev, M. K. Leont’ev, and I. L. Gladkii p. 810  abstract

AIRCRAFT PRODUCTION TECHNOLOGY

Electrolytic-Plasma Jet Polishing of Additively Manufactured Gas Turbine Engine Components

K. Yu. Nagulin, A. A. Terent’ev, M. D. Belov, and A. Kh. Gil’mutdinov p. 822  abstract

Mathematical Description of Physical and Chemical Processes Occurring during the Application of Polymer Powder Coatings by Jet Methods

V. L. Fedyaev, E. R. Galimov, and A. V. Belyaev p. 831  abstract

Problem Description and a Study of Reinforcement Components to Produce Composite Hybrid Structures

V. I. Khaliulin, V. V. Batrakov, and P. A. Petrov p. 843  abstract

RADIO ENGINEERING AND COMMUNICATION

Algorithm for Assessing the Technical Condition of the Monitoring Radar Based on the Clustering of Multidimensional Nonuniform Time Series

A. V. Timoshenko, V. I. Goncharenko, A. Yu. Perlov, and V. A. Pankratov p. 855  abstract

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

A Research of Interference between Elements of a Helicopter Fuselage with a Wing

A. S. Batrakov, and V. V. Pakhov p. 863  abstract