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Научный вестник МГТУ ГА
ISSN 2079-0619 · Moscow State Technical University of Civil Aviation · 1.272 artikel di indeks
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Artikel Jurnal
Canard surface role estimation for aircraft of the canard layout
The range of subsonic speeds is considered. The research of interference of the front and rear load-bearing surfaces is focused on the assessment of two factors: the degree of lift increasing of the wing-canard system due to the positive canard surface lift force and the role of this force in the…
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Artikel Jurnal
On the issue of creating a basic list of hazards associated with the activities of the developer of a promising supersonic civil aircraft
Currently, Russia has various documents, approved by government decrees, aimed at improving regional air transport connectivity and population mobility. One of the ways to address this issue could be the development of a new supersonic civil aircraft. Among the many challenges associated with the…
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Artikel Jurnal
Morphing wing airfoil optimization for small unmanned aviation vehicle
Modern small unmanned aerial vehicles (UAVs) perform a wide range of missions, requiring high efficiency in various, often conflicting, flight conditions. Conventional airfoils, optimized for a single specific condition, exhibit suboptimal performance in others, limiting the overall flight…
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Artikel Jurnal
Experimental investigation and optimization of a check filter element for the dynamic measurement method of aviation fuel industrial cleanliness level
Ensuring the cleanliness of aviation fuel from mechanical impurities is a critical factor in flight safety. Existing laboratory methods for monitoring fuel cleanliness are discrete and do not allow for the prompt detection of contaminants during aircraft refueling, which creates significant risks…
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Artikel Jurnal
Aircraft vortex wake detection based on airflow skew data using gradient optimization methods
This paper studies the problem of automatic detection of stable vortex wake generated by fixed-wing aircraft using airflow skew vectors measurements. A methodological approach is proposed that enables the effective application of gradient optimization methods to solve this problem. To smooth the…
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Artikel Jurnal
Engineering aviation service of the civil aviation: from technical operation to continued airworthiness (part 2)
The article continues and develops the subject of the civil aviation engineering service in the 75th anniversary year of its existence, raised in the first article on this theme. It analyzes the activities of the aviation engineering service in the early post-Soviet period, when the main regulatory…
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Artikel Jurnal
Optimization of the approach to Moscow Flight Information Region: Environmental and economic aspects of implementing the continuous descent procedure
With the growth of air traffic, the implementation of environmentally friendly and cost-effective technologies in civil aviation becomes increasingly important. One promising solution is the Continuous Descent Operations (CDO) mode, which ensures an optimal descent trajectory, reducing fuel…
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Artikel Jurnal
Routing of cargo unmanned aerial vehicles in remote areas. Part 1
A serious problem in the Russian Arctic, which can be solved through the use of unmanned aerial vehicles (UAVs) given the lack of year-round road access, remains the delivery of goods and the patrolling of forests to identify and monitor the development of wild fires. This article is devoted to the…
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Artikel Jurnal
Application of simulation models of the hydraulic system and flight control actuators in aircraft operation
The paper considers the application of a simulation model of the hydraulic system and actuation devices of the flight control system during aircraft operation. The relevance of using simulation models in aircraft operation or design is formulated. The results of developing Simulink-models of the…
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Artikel Jurnal
Numerical study of helicopter airframe aerodynamics combined with coaxial main rotor using the URANS method
The work is dedicated to numerical modeling of Kamov Ka-226 helicopter aerodynamics for isolated helicopter airframe and helicopter airframe with coaxial main rotor. The CFD (computational fluid dynamics) method based on the URANS approach (Unsteady Reynolds-averaged Navier-Stokes equations) based…
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Artikel Jurnal
An algorithm for creating adaptive exercise scenarios on a simulator using dynamic complexity to improve the effectiveness of ATCO training
This work is devoted to the development of an innovative algorithm for creating adaptive simulator scenarios for training air traffic control (ATC) officers using dynamic complexity. The relevance of the study is caused by the rapid increase in air traffic intensity, which requires fundamentally…
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Artikel Jurnal
The flow part comparative analysis of a gas turbine engine intermediate casing with a starter generator integrated onto the rotor shaft
The paper presents a flow part comparative analysis of a gas turbine engine intermediate casing with a starter-generator integrated onto the rotor shaft based on a more electric aircraft engine concept. This paper identified the need for design modifications and a gas-dynamic study of the…
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Artikel Jurnal
Methodological foundations for ensuring aircraft flight safety under the influence of coherent vortex structures
This paper presents the methodological foundations for solving the problem of flight safety for tactical and operational aviation aircraft under the influence of coherent vortex structures in the atmosphere during the most critical flight phases: takeoff and landing at joint-use airfields…
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Artikel Jurnal
Methods for determining the stiffness properties of a helicopter main rotor blade based on computational experiments
Due to the widespread use of composite materials in the designs of helicopter main rotor blades (MRB), special attention should be paid to monitoring the obtained stiffness characteristics at all stages of their development and operation. The available experimental control methods have inherent…
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Artikel Jurnal
The use of onboard decimeter-band radar stations for humanitarian demining
Humanitarian demining is a pressing issue today. This paper examines various technical means used in engineer reconnaissance to detect mines and substantiates the need for radar support for humanitarian engineer reconnaissance. An airborne engineer reconnaissance radar system based on a…
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Artikel Jurnal
Modelling and analysis of defect rectification impact on turbofan engine compressor blades’ operation capacity
Jet engines are subject to various damaging factors, among which operational ones are dominant throughout their life cycles. At the same time, the dominant share of deteriorations specific to compressor components occurs in the fan module of modern turbofan engines: bends, cracks as well as dents…
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Artikel Jurnal
Protection of corporate information systems of aviation enterprises from zero-day attacks: an intrusion detection approach based on deep unsupervised learning
The paper considers the urgent task of detecting zero-day attacks in corporate information systems of aviation enterprises classified as critical information infrastructure (CII). It is shown that traditional signature-based protection tools, including classical intrusion detection systems (IDS)…
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Artikel Jurnal
Statistical modeling of combat functioning for army aviation airborne complexes system
The development of mathematical models of the combat functioning of army aviation aircraft complexes is the most important task in the field of researching the prospects for the development of aviation technology and substantiating requirements for it. One of the main requirements for these models…
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Artikel Jurnal
A new model of higher education: Issues and prospects for training personnel for the air transport industry
This paper considers the main issues related to the training of specialists for civil aviation at the higher educational institutions of Russia, which are caused by the reorganization of the national education system. Based on an analysis of the scientific publications and discussions among…
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Artikel Jurnal
Comparative study of required power of coaxial rotor and equivalent single rotor at the hover and forward flight modes
A coaxial main rotor (MR), consisting of upper (UR) and lower (LR) rotors with a spacing of planes and a different direction of rotation, has a number of advantages in aerodynamic characteristics compared to an equivalent single rotor of the same radius, having a double number of blades and…
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