Contents

Russian Aeronautics

Vol. 65, No. 3, 2022

AIRCRAFT EQUIPMENT

Estimation of the Required Voltage and the Effect of Joule Heating on the Implementation Efficiency of the Thermionic Cooling of Aircraft

A. V. Kolychev, P. A. Arkhipov, V. A. Kernozhitskii, and M. V. Chernyshov p. 439  abstract

FLIGHT VEHICLE DESIGN

Conceptual Assessment of New Helicopter Project Solutions Based on the Take-off Mass Sensitivity Analysis

Pinqi Xia, and A. S. Kretov p. 446  abstract

STRUCTURAL MECHANICS AND STRENGTH OF FLIGHT VEHICLES

Free Oscillations of a Cylindrical Shell

S. D. Algazin p. 461  abstract

Application of the Boundary Element Method to Solving the Plane Elastic Problems

A. F. Garif’yanov, and R. Sh. Gimadiev p. 467  abstract

Thermal Mode of Two-Layer Heat-Protective Coating of a Ballistic Capsule When It Is Returning to the Earth with Parabolic Velocity

V. S. Zarubin, V. N. Zimin, V. V. Leonov, and V. S. Zarubin p. 474  abstract

Accounting for Concentrated Weights in the Equations of Blade Bending in Two Planes and Torsion

E. I. Nikolaev, S. E. Nikolaev, and A. Z. Voronkov p. 483  abstract

Vibration Transmission in Thin-Wall Framed Structures

V. N. Paimushin, V. A. Firsov, V. M. Shishkin, and R. K. Gazizullin p. 490  abstract

FLIGHT DYNAMICS AND CONTROL OF FLIGHT VEHICLES

Multimodal Interface Architecture for Unmanned Aerial Vehicle Control

N. S. Abramov, Yu. G. Emel’yanova, A. A. Talalaev, V. P. Fralenko, and M. V. Khachumov p. 498  abstract

Features of the Formation of Temporary Clusters of Spacecraft Monitoring Radio Emission Sources on the Earth Surface

N. F. Averkiev, V. V. Salov, and A. Yu. Khasanov p. 507  abstract

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

Investigation of the Characteristics of Airfoils with Air Suction from the Upper Surface and a Given Pressure Distribution

P. V. Bulat, N. V. Prodan, S. Yu. Dudnikov, and A. A. Kurnukhin p. 515  abstract

Selection of the Optimal Airfoil for the Small-Sized Unmanned Helicopter Main Rotor Blade

K. S. Vasil’chenko, S. V. Reznik, N. L. Aung, and A. R. Gareev p. 524  abstract

Flow Features and Aerodynamic Analysis of the Canard Missiles

V. T. Kalugin, S. N. Voropaev, and D. K. Nazarova p. 533  abstract

Computation of the Added Masses of Bodies by Using T-Schemes for Numerical Reconstruction of the Vortex Sheet Intensity

I. K. Marchevskii, and G. A. Shcheglov p. 541  abstract

AIRCRAFT AND ROCKET ENGINE THEORY

Conceptual Design and Preliminary Calculations of a Hybrid Power Plant on Liquid Hydrogen for a Regional Aircraft

A. N. Varyukhin, V. A. Kaderov, N. A. Malevich, M. A. Ovdienko, Yu. A. Ravikovich, and A. A. Fedorov p. 550  abstract

A Technique to Estimate the Output of the Fluid Jet Pump Supply from a Tank Placed in a Deep Mine

G. L. Degtyarev, N. N. Elyukin, V. I. Kiselev, and A. S. Meshchanov p. 561  abstract

On the Mechanisms of Pulsed Combustion Initiation in a Valveless Ejector Bypass Pulsed Air-Jet Engine

K. V. Migalin, and K. A. Sidenko p. 568  abstract

AIRCRAFT INSTRUMENTS AND INSTRUMENTATION COMPUTER COMPLEXES

Electronic System of Spatial Measurement of Air Parameters of the Aircraft Motion with the Fixed Receiver of Incident Flow

E. S. Efremova, B. I. Miftakhov, V. V. Soldatkin, and V. M. Soldatkin p. 575  abstract

Improvement of Application Efficiency for Li-Ion Batteries Used in the Satellite Electric Power Subsystems

M. V. Nesterishin, V. G. Bukreev, R. L. Kozlov, and A. V. Zhuravlev p. 582  abstract

AIRCRAFT PRODUCTION TECHNOLOGY

Modeling and Optimization of Manufacturing Processes of the Hybrid Composite Propeller Blade

E. A. Puzyretskii, L. P. Shabalin, D. V. Savinov, and I. V. Mareskin p. 590  abstract

Integral Quality Estimation of the Explosive Forming Blank for the Titanium Alloy Front Bottom of the Solid Propellant Rocket Engine

F. A. Urazbakhtin, and V. F. Urazbakhtin p. 600  abstract

RADIO ENGINEERING AND COMMUNICATION

Numerical Simulation of Convective Heat Transfer under Forced Motion of Heat Carrier in Cooling Systems with Split Fin

A. A. Lopatin, R. A. Gabdullina, A. R. Biktagirova, and A. A. Terent’ev p. 610  abstract

STRUCTURAL MECHANICS AND STRENGTH OF FLIGHT VEHICLES

Diagnostics of Distributed Mechanical Impact by Indicator Polymer Coating

A. A. Pan’kov p. 618  abstract

AIRCRAFT PRODUCTION TECHNOLOGY

Increasing the Lifetime of Gas Turbine Engine Parts Operating under Fretting Conditions

I. R. Aslanyan, M. S. Eremkina, and D. D. Korolev p. 623  abstract