Aerospace engineering and technology


ISSN (online):
 2949-401X

Media registration certificate: ЭЛ № ФС 77 - 85225 от 25.04.2023


Scientific and Technical Journal “Aerospace Engineering and Technology” publishes original scientific articles and review papers containing new results of fundamental, applied and developmental research of theoretical, applied and experimental nature related to the development of aerospace equipment, technologies of its production and operation.

The mission of the journal is the rapid spreading of new scientific knowledge and advanced methods in the area of national aerospace industry.

Founder & Publisher

Baltic State Technical University “VOENMEH”

Editor-in-Chief

Mikhail Chernyshov, Doctor of Engineering Sciences, Corresponding Member of the Russian Academy of Rocket and Artillery Sciences, Professor of “Plasma, Gas Dynamics and Heat Engineering” Department, Faculty of Rocket and Space Engineering, Baltic State Technical University “VOENMEH”

Frequency / Assess

4 issues per year / Open

Website:

http://aerocosmtech.ru/

 

 

 

 

 


Current Issue

Vol 3, No 4 (2025)

Cover Page

Full Issue

AIR, GAS DYNAMICS AND HEAT EXCHANGE

Research and development of adaptive wings
Amelyushkin I.A., Druzhinin O.V.
Abstract
The study presents new structural designs of adaptive wings and evaluates their aerodynamic benefits. A comparative analysis and a concise review of existing adaptive wing concepts were carried out. The investigation included determining the variation of the center of pressure along the wing chord with changes in the angle of attack. The results were compared with those for a conventional high-lift wing and a clean wing profile. The obtained data can be applied to the design of short takeoff and landing (STOL) aircraft to enhance overall aerodynamic efficiency and control performance.
Aerospace engineering and technology. 2025;3(4):552-562
pages 552-562 views
Semi-analytical modeling of wave and jet flows in a stratified fluid
Makarenko N.I., Maltseva J.L.
Abstract
Two classes of nonlinear problems concerning wave and jet structures in steady flows of an inhomogeneous fluid are considered. One of them is related to the modeling of lee waves in atmospheric airflows over uneven terrain. The other group of problems concerns the description of internal waves in deep-ocean currents. A common feature of both cases is the combined use of analytical approaches and computer algebra methods to construct asymptotic solutions of the equations of motion of a stratified fluid. The first approximate model is employed for the numerical calculation of jet-flow patterns and the nonlinear interference of lee waves over complex topography. The second model is used to characterize the qualitative properties and parameters of solitary internal waves in layered weakly stratified near-bottom flows.
Aerospace engineering and technology. 2025;3(4):563-583
pages 563-583 views
Numerical study of the influence of passive blowing on the aerodynamic characteristics of a high-lift airfoil in dry and humid air
Brutyan M.A., Pavlenko O.V., Htun Y.
Abstract
Interest in various active and passive methods of flow control over an airfoil, aimed at increasing the maximum lift coefficient of a wing, is driven by the relevance of reducing take-off and landing distan- ces. Unlike active flow control methods, which require energy input, passive methods use the energy of the external airflow in such a way as to produce an overall beneficial effect. Passive flow control methods are simpler than active ones, have more reliable designs, and generally add little extra weight. This work presents a passive method for controlling the flow over a high-lift wing airfoil with a flap by means of specially profiled flow channels. The described control method is effective both with the flap undeflected (cruise flight mode) and with the flap deflected. It is shown that in the profiled channel the airflow accelerates and exits tangentially onto the upper surface of the flap, increasing suction and shifting the boundary-layer separation line on the deflected flap downstream. Humid air with increased moisture concentration raises the momentum coefficient of the blown jet.
Aerospace engineering and technology. 2025;3(4):584-597
pages 584-597 views

ENGINE AND POWER PLANTS

Competing Flames Model Applied to Pasty Propellants
Babuk V.A., Burachek E.S.
Abstract
The article examines approaches to modeling the combustion process of high-energy pasty propellants. A physical picture of the combustion process is presented. A mathematical framework is developed that accounts for the influence of the thickness and porosity of an intermediate structure in the combustion zone – the skeleton layer (SL). A multi-parameter optimization problem is formulated as a tool for the study. A sequence for applying the optimization procedure to propellant formulations is defined, taking into account the specific features of their combustion processes. Simulation results are obtained that confirm the validity of the adopted assumptions. Directions for further research are identified.
Aerospace engineering and technology. 2025;3(4):598-613
pages 598-613 views

MECHANICS OF DEFORMABLE SOLIDS, AEROELASTICITY PROBLEMS

Prediction of critical crack opening and crack-tip stresses in polymer structural elements of unmanned aerial vehicles considering creep
Andryushkin A.Y., Kazakova A.O., Romanat N.I.
Abstract
Thermoplastics are widely used in the manufacturing of structural components for unmanned aerial vehicles (UAVs). Under sustained and variable loading, polymers exhibit creep, which significantly affects crack development. Therefore, determining critical crack opening and stresses acting at the crack tip, with consideration of material creep, is of practical importance. The study presents formulas for evaluating the mechanical properties of a polymer over time under creep conditions. A methodology for calculating crack opening in a polymer plate subjected to stresses acting in the near-tip region has been developed using the boundary element method. It has been established that critical crack opening is characterized by the condition Dymax ≥ DC, where Dymax and DC denote the maximum and critical crack opening, respectively. The practical significance of the proposed methodology is demonstrated through the calculation of crack opening and crack-tip stresses in a polypropylene plate under creep conditions.
Aerospace engineering and technology. 2025;3(4):614-627
pages 614-627 views

AIRCRAFT FLIGHT CONTROL

Method for constructing spatial trajectory and motion of a maneuvering aircraft
Pravidlo M.N., Biryukov P.A., Yurlovsky A.F.
Abstract
Methods for constructing complex flight trajectories of aircraft are analyzed, and the specific features of their formation are examined. A universal algorithm is proposed for generating an arbitrary spatial trajectory for a maneuvering aircraft in simulation tasks. The algorithm involves forming a sequence of motion segments that implement elementary maneuvers. Possible variants of the algorithm's construction, as well as limitations and extensions in its implementation, ar discussed.
Aerospace engineering and technology. 2025;3(4):628-641
pages 628-641 views
Pathways to enhancing UAV autonomy in emergency situations
Syrovoy G.V., Pobeda T.V., Atroshenko D.V.
Abstract
The article examines current approaches to enhancing the autonomy of unmanned aerial vehicles (UAVs) under emergency conditions. The importance of UAV autonomy for the effective execution of search-and-rescue, monitoring, and emergency recovery operations in disaster zones is substantiated, where traditional methods are often impractical due to high risk to personnel and limited access to incident sites. An analysis of modern technological solutions is conducted, including computer vision systems with AI algorithms, multi-sensor navigation complexes, onboard computing platforms, and algorithms for route and energy optimization. Based on studies from 2022–2025, the effectiveness of LiDAR systems, modular navigation interfaces, and edge-computing technologies is evaluated. Key limitations are identified, such as dependence on satellite navigation, vulnerability of communication channels, limited energy resources, and restricted computational capacity of onboard systems. The following development directions are proposed: integration of quantum sensors, adoption of hybrid power systems, and use of adaptive algorithms for collective swarm behavior of UAVs. Recommendations are formulated for standardizing autonomy requirements for UAVs in emergency situations and for establishing testing grounds to validate operational scenarios. It is shown that a comprehensive approach to enhancing autonomy can yield a manifold increase in the responsiveness and safety of emergency rescue operations.
Aerospace engineering and technology. 2025;3(4):642-653
pages 642-653 views

AIRCRAFT DESIGN, CONSTRUCTION AND MANUFACTURING

Computational determination of parameters of evolving porous media in unidirectional composite materials
Nilov A.S., Butorina I.A., Mokhova E.A.
Abstract
This paper presents methods for calculating the parameters of the porous medium in unidirectional composite materials (CMs) with various types of regular (hexagonal and tetragonal) and irregular fibrous structures. The porous medium is represented as a system of inter-bundle and intra-bundle pores. These calculation methods can be considered as elements for describing the initial and current structure of CMs when modeling chemical vapor infiltration (CVI) processes of fibrous preforms during the fabrication of composite materials with carbon and ceramic matrices.
Aerospace engineering and technology. 2025;3(4):654-671
pages 654-671 views
Non-destructive testing methods for determining thermophysical properties of materials
Brovka G.P., Lysenko S.A., Agutin K.A., Murashko A.A., Brovka A.G.
Abstract
The article substantiates two non-destructive testing methods — non-contact and contact — designed to determine the thermophysical properties of materials by locally heating a semi-infinite medium using a disk-shaped heat source. During processing of the heating thermogram obtained with a non-contact source, the homochronicity parameter is used, defined as the ratio of the average rates of surface temperature change taken from different sections of the heating thermogram. It is established that, for certain geometric dimensions of the heat source and temperature measurement points, the homochronicity parameter ε is functionally related to the product of the material's thermal diffusivity and the temperature measurement time. This makes it possible, using nomograms derived from preliminary numerical calculations for a series of materials with known thermophysical properties, to determine the thermal diffusivity and thermal conductivity coefficients of the test materials without employing complex methods for solving inverse heat conduction problems. The contact method involves time-resolved detection of the excess temperature at the center or at a certain distance from the disk-shaped heat source, and interpretation of the temperature profile using nomograms obtained with consideration of the heater's heat capacity and the homochronicity parameter values, or by means of a neural network that establishes a relationship between the heating thermogram parameters and the target thermophysical properties.
Aerospace engineering and technology. 2025;3(4):672-687
pages 672-687 views

AEROSPACE COMMUNICATIONS AND INFORMATION

Development of a compact, high-speed microwave frequency synthesiser with low phase noise
Sotnikova N.V., Konoplev Y.V., Motovilov A.O.
Abstract
This work addresses the problem of creating a compact, high-speed, low-noise microwave frequency synthesizer. A solution is proposed in the form of a detailed description of a promising synthesizer architecture. Brief information is provided on the main frequency synthesis methods, and the advantages and disadvantages of each method are analyzed. A definition of the hybrid frequency synthesis method is formulated. Computer simulation results are presented that confirm the advantages of a hybrid architecture combining phase-locked loop (PLL) and direct digital synthesis (DDS) techniques, enabling signal generation over a wide frequency range while achieving low phase noise and preserving high speed and other benefits.
Aerospace engineering and technology. 2025;3(4):688-701
pages 688-701 views