Contents

Russian Aeronautics

Vol. 68, No. 2, 2025

FLIGHT VEHICLE DESIGN

Modeling of the Stress-Strain State of Load-Bearing Structures in Abaqus and MeshFree Software Systems at the Stage of Design of Aviation Equipment Products

L. I. Mironova and S. M. Koval’ p. 255  abstract

STRUCTURAL MECHANICS AND STRENGTH OF FLIGHT VEHICLES

Non-Destructive Buckling Experiments by Static Method

R. S. Abdullin, A. A. Ivanov, and V. I. Kiselev p. 266  abstract

Three-Layer Structural Elements of Aviation and Space Technology. Methodology for Constructing Models of Layer-by-Layer Finite Element Analysis of the Stress-Strain State of Irregular Three-Layer Shells, Including Those with Rectangular Cutouts

V. N. Bakulin p. 274  abstract

Strength-Based Design Constraints for Optimizing the Anisotropic Medium-to-Thick Composite Panels in Aircraft Structures

L. M. Gavva and T. A. Han p. 283  abstract

A Multi-Layer Soft Shell under the Action of Blast Wave

R. Sh. Gimadiev, V. I. Khaliulin, and A. F. Garif’yanov p. 296  abstract

Experimental Study of Polymer Composite Materials for Fire Resistance and Fire Proofness

G. A. Glebov, D. S. Kirichenko, and A. S. Sabitov p. 305  abstract

Radio-Transparent High-Temperature Composite Materials for the Manufacture of High-Tech Products for Aerospace Industry

E. R. Zhdanov, A. V. Kryukov, O. S. Kharina, D. S. Stepynin, and A. V. Volkov p. 311  abstract

Artificial Neural Network as a Tool for Predicting the Technical Condition of Rotary-Wing Aircraft Components

B. B. Safoklov and S. A. Serebryanskii p. 316  abstract

FLIGHT DYNAMICS AND CONTROL OF FLIGHT VEHICLES

Determination of the Optimal Control Law for the Thrust Vector of an Active-Reactive Type Space Penetrator

E. V. Gusev, V. A. Zagovorchev, V. V. Rodchenko, E. R. Sadretdinova, and E. A. Shipnevskaya p. 327  abstract

Stabilizing the Orbital Orientation of a Spacecraft at Measuring only Angular Rates of Roll and Pitch or Angular Rates of Yaw and Pitch

N. E. Zubov, A. V. Lapin, and V. N. Ryabchenko p. 334  abstract

Virtual Model of a Highly Maneuverable Aircraft Dynamics

A. Z. Tarasov and V. N. Tikhonov p. 347  abstract

Synthesis of Proportional-Integral-Derivative Guidance Law for Homing Missiles Using the PSO Algorithm

Cao Huu Tinh and Vu Xuan Thin p. 356  abstract

Experimental and Numerical Investigation of Trailing Edge Wing Morphing to Improve the Aerodynamic Performance and Stability Characteristics of a Fixed Wing UAV

S. Babu, L. Livin, L. Prawin, S. Venkatachalam, and A. R. Rajendran p. 364  abstract

Supersonic Flow past a Bi-Conic Nose Cone: A Computational Parametric Study

A. Narayan, S. Kumar, H. Raza, M. Kumar, G. S. Reddy, and R. Kumar p. 378  abstract

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

A New Exact Solution of the Navier–Stokes Equations for Describing the Unsteady Flows of Vertically Swirled Fluid

E. Yu. Prosviryakov, L. S. Goruleva, and O. A. Ledyankina p. 393  abstract

AIRCRAFT AND ROCKET ENGINE DESIGN AND DEVELOPMENT

Distribution Laws for Random Diagnostic Parameters of Spark Discharges in Semiconductor Spark Plugs of Capacitive Ignition Systems

F. A. Gizatullin and O. A. Yushkova p. 402  abstract

Decision Support at the Initial Stage of Turbofan Engine Design

I. A. Krivosheev, K. E. Rozhkov, N. B. Simonov, and O. N. Ivanova p. 409  abstract

Low-Emission Combustors for Aircraft Engines: Development and Numerical Analysis of Technical Concepts Using the Reduced Kinetic Mechanism

A. N. Tarasenko, A. Yu. Vasil’ev, B. I. Loukhovitski, A. S. Sharipov, and M. V. Siluyanova p. 423  abstract

AIRCRAFT AND ROCKET ENGINE THEORY

Cutback of Trailing Edge of a Fan-Shaped Hole Contributing to the Film Cooling Effectiveness at a Blowing Angle of 45 deg

E. Yu. Marchukov, A. V. Il’inkov, A. V. Shchukin, V. V. Takmovtsev, and K. V. Kakhovskii p. 433  abstract

AIRCRAFT INSTRUMENTS AND INSTRUMENTATION COMPUTER COMPLEXES

Algorithm for Synthesis of Relief Surface with Given Fractal Dimension Based on Fractional Dimension Operators

Yu. K. Evdokimov, L. Yu. Fadeeva, and D. V. Shakhturin p. 442  abstract

Development of an Algorithm for Absolute Visual-Inertial Navigation of Unmanned Aerial Vehicles

P. A. Lazareva, A. I. Malikov, G. L. Degtyarev, and R. T. Mannanov p. 449  abstract

Models of Dynamic Characteristics and Errors of Instrumentation Channels of the Air Data System with the Fixed Flush-Mounted Flow Receiver

V. M. Soldatkin, V. V. Soldatkin, E. S. Efremova, A. V. Nikitin, R. V. Kozlovskii, and G. V. Kozlovskii p. 456  abstract

AIRCRAFT PRODUCTION TECHNOLOGY

Epoxy Polymer Based Foam Fillers and Sandwich Structures with a Core Based on Them

A. Kuomalibieke, D. M. Usmanov, N. D. Startsev, K. A. Andrianova, and L. M. Amirova p. 463  abstract

Implementation of Vacuum Forming Technology in the Production of Thin-Walled High-Temperature Radio-Transparent Composite Structures

P. L. Lyudogovskii, A. V. Naumov, and N. V. Semin p. 471  abstract

Synthesis of Exfoliated Graphite and Study of Its Electrical Conductivity in the Composition of Active Masses of Three-Dimensional Electrodes for Supercapacitors

M. V. Morozov, S. V. Drobyshev, D. N. Zhukova, V. V. Kuznetsova, D. N. Morozov, and E. A. Solov’ev p. 477  abstract

RADIO ENGINEERING AND COMMUNICATION

Modeling of Onboard Cable at Cryogenic Temperatures and under Vacuum Conditions

S. V. Efremov, V. P. Zdornikova, A. P. Leonov, and O. V. Sapugol’tseva p. 485  abstract

Mathematical Modeling of Identification of the Avionics Antennas Topology on the Airframe

V. N. Nikolaev p. 492  abstract

Analysis of Effectiveness of Methods of Protection against Interference Emission from Stationary Plasma Thrusters in Deep-Space Communication Systems

P. S. Tyapkin, N. A. Vazhenin, and A. P. Plokhikh p. 501  abstract

Analysis of the Possibility of Using Discrete Beam Hopping of an Active Phased Antenna Array to Establish the Information Exchange in Heterogeneous Communication Networks

G. V. Chechin, V. E. Kolesnichenko, and I. A. Zhuchkov p. 508  abstract

AIRCRAFT AND ROCKET ENGINE DESIGN AND DEVELOPMENT

Methodology for Selecting Optimal Parameters of the Afterburner Chamber of an Aircraft Ramjet Power Plant Based on Ballistic Efficiency Criteria

V. V. Vetrov, P. D. Shilin, and A. S. Fedorov p. 516  abstract

AIRCRAFT AND ROCKET ENGINE THEORY

Influence of Air Excess Ratio and Acoustic Tuning on the Operation Process of the Ejector Pulsejet Engine

K. A. Sidenko and V. V. Biryuk p. 522  abstract

AIRCRAFT PRODUCTION TECHNOLOGY

Methodology of Forming the Knowledge Base of the Intelligent Process Design System

E. I. Egorova, A. N. Lunev, and D. V. Kurylev p. 527  abstract