Contents

Russian Aeronautics

Vol. 65, No. 1, 2022

AIRCRAFT EQUIPMENT

Analysis of Conditions of Oscillating Onset in Aircraft Fuel Supply Systems

A. L. Lyutov, M. B. Novozhenin, and V. A. Ogorodov p. 1  abstract

FLIGHT VEHICLE DESIGN

Application of Integrated Layout for ”Cryogenic“ Transport Category Aircraft

A. S. Kretov, and V. V. Glukhov p. 10  abstract

STRUCTURAL MECHANICS AND STRENGTH OF FLIGHT VEHICLES

Special Features of Measuring the Elastic Strains by Fiber Optical Sensors of the Spacecraft

M. A. Ledyankin, A. M. Girfanov, and T. A. Agliullin p. 25  abstract

Theoretical-Experimental Study of Sound Wave Passage through a Double Obstacle

V. N. Paimushin, V. A. Firsov, and R. K. Gazizullin p. 32  abstract

Development and Numerical Justification of the Specimen for the Surface Crack Growth Rate Tests

M. M. Yakovlev, R. R. Yarullin, and A. P. Zakharov p. 41  abstract

FLIGHT DYNAMICS AND CONTROL OF FLIGHT VEHICLES

Development of an Approach to the Formation of Dynamic Models of the Process of Transformable Space Structures Deployment

V. N. Bakulin, and S. V. Borzykh p. 49  abstract

Identification of Aerial Objects during Detection and Tracking by the All-Atmosphere Radar

S. F. Boev, A. V. Timoshenko, S. N. Razin’kov, and V. A. Shevtsov p. 57  abstract

Robotic Controlled Electromechanical Model of Two Links of Variable Length for Aerospace Purposes

A. V. Borisov, I. E. Kaspirovich, R. G. Mukharlyamov, and K. D. Filippenkov p. 68  abstract

Algorithm of Unmanned Aircraft Attitude Estimation in the Case of Moderate Requirements to the Onboard Processor Computing Resources

T. Yu. Gainutdinova, A. V. Gainutdinova, V. G. Gainutdinov, M. V. Trusfus, and I. N. Abdullin p. 81  abstract

Influence of Motion Cues on a Landing Performance in Conditions of the High Atmosphere Turbulence

A. V. Efremov, M. S. Tyaglik, I. Kh. Irgaleev, T. V. Voronka, and A. S. Tyaglik p. 89  abstract

Analytical Synthesis of Stabilization Laws of Coupled Motions of an Aircraft in the Pitch–Yaw Channels in the Absence of Information about the Angle of Attack

N. E. Zubov, V. N. Ryabchenko, and A. V. Lapin p. 99  abstract

Statistical Parametric Design of a Controller in the Stabilization Loop of a Single Axis Gyro-Stabilized Platform Using Stochastic Global Optimization Methods

K. O. Lukin, and S. V. Krivosheev p. 111  abstract

Mission Performance Analysis for a Piston-Engined Ultralight Unmanned Helicopter

Yu. P. Onushkin, D. A. Sizov, and A. V. Ostrovoi p. 121  abstract

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

Lift Generation Effect in Aerodynamic Layouts with a Submerged Air Intake Device and an Upper Planing Step

M. V. Ambrozhevich, A. S. Kartashev, A. V. Kornev, and V. A. Sereda p. 132  abstract

Algorithm for Determining the Aerodynamic Performance by the Flight Test Results

S. A. Mikhailov, A. A. Makhan’ko, and M. A. H. Hamzah p. 140  abstract

Vortex Core Localization Using Velocity Gradients

R. P. Stepanov, A. N. Kusyumov, and G. Barakos p. 149  abstract

Interaction of a Preloaded Elastic Shell of Revolution with a Shock Wave in a Liquid

I. K. Turkin p. 156  abstract

About the Use of Vortex Generators to Improve Aircraft Aerodynamics

V. G. Tsipenko, and V. I. Shevyakov p. 165  abstract

AIRCRAFT AND ROCKET ENGINE DESIGN AND DEVELOPMENT

Boosting the Combustion Process in an Ejector Bypass Pulsating Airbreathing Jet Engine

K. V. Migalin, and K. A. Sidenko p. 173  abstract

AIRCRAFT AND ROCKET ENGINE THEORY

The Influence of Flow Regulator Dynamics on the Internal Ballistic Parameters of Multi-Nozzle Solid Propellant Propulsion. Results of Numerical Modeling

S. A. Bitkin, N. N. Elyukin, M. A. Korepanov, and A. I. Karpov p. 180  abstract

AIRCRAFT INSTRUMENTS AND INSTRUMENTATION COMPUTER COMPLEXES

Influence of Manufacturing Tolerance on Aerodynamic Performance and Errors of the Multifunctional Air Pressure Receiver of Aircraft Aerometric Systems

V. P. Derevyankin, A. A. Pavlovskii, V. V. Soldatkin, and V. M. Soldatkin p. 186  abstract

AIRCRAFT PRODUCTION TECHNOLOGY

Suspended Kinetic Energy Storage Based on High-Temperature Superconductors

V. A. Podguzov, D. V. Rusanov, and D. V. Golovanov p. 193  abstract

AIRCRAFT EQUIPMENT

Acoustic Interaction of Piezo-Adaptive Resonance Cells of the Sound-Absorbing Honeycomb Panel

P. V. Pisarev, A. A. Pan’kov, and A. N. Anoshkin p. 200  abstract

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

Numerical Simulation of the Flow around the Fuselage of Promising High-Speed Helicopter

A. S. Batrakov, and V. V. Pakhov p. 206  abstract

On a Nonclassical Approach to Constructing Self-Similar Solutions in the Laminar Boundary Layer Theory

K. G. Garaev p. 213  abstract

AIRCRAFT PRODUCTION TECHNOLOGY

Application of Polymer Resin to the Surface of Fabrics in the Manufacture of Aircraft Parts

M. S. Salina, O. G. Zakharov, and Yu. P. Kataev p. 219  abstract

Erratum

Erratum to: Influence of Frequency Modulation Caused by the Onboard Radio Signal Reflection from the Helicopter Blades on the Aerodrome Automatic Direction Finders Accuracy

G. K. Aslanov, T. G. Aslanov, R. B. Kazibekov, and R. R. Musaibov p. 224  abstract