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Active Generation of Lift Force in the “Wing–Ejector” Integral Aerodynamic Configuration
AbstractThe effect of active generation of lift force by an electric impeller propulsion system in integral aerodynamic configurations of vertical...
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Numerical Investigation to Study the Effects of Wing Flexibility on the Store Trajectory Using MSC CoSim
Traditional flight testing and wind tunnel testing require expensive resources in terms of time and cost. Safety and cost concerns in the testing of...
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Optimization of Design Parameters of a Small-Sized Unmanned Aircraft with a Turbojet Engine Equipped with an Ejector Thrust Magnifier
In this article, the object of research is various layouts of unmanned aerial vehicles with a small turbojet engine using an ejector thrust...
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Hyplane: a single-stage suborbital aerospaceplane
This paper has the aim to report the status of the HYPLANE project to date. HYPLANE is a horizontal take-off and landing Mach 4.5 bizjet-size...
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Designing a Basic Model of an Unmanned Aerial Vehicle for the Subsequent Development of a Family of Samples with Different Purposes
The general initial positions making basis of technical intention of the maneuverable multimode unmanned aerial vehicle, that determined forming the...
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Control of Wing-Engine-Slat Cut Out Flow Separation Using Nacelle Nozzle Modification
A numerical study on active flow control (AFC) to a swept wing in a take-off configuration was conducted. The focus of this study is the feasibility...
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Analysis on Architecture Design and Evaluation Technology of Civil Aircraft Fuel System
Based on the fuel system architecture of civil aircraft, this paper forms the ability to establish the design and evaluation of aircraft fuel system...
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Smart Design and Optimization of a Universal and Low-Cost Double-Tailed UAV
Many kinds of UAV have been designed as universal platforms today, for the use of cargo, monitor, even bomber during the Russo-Ukrainian War, but it...
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Realization of Dual-Mode Combustion by Changing the Geometry of the Model Combustion Chamber Flow Part of a Ramjet Engine
AbstractThis paper presents the results of experiments on the methane-hydrogen mixture combustion in a test bench model of a dual-mode wide-range...
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Enhancement of signal-to-noise ratio of schlieren visualization measurements in low-density wind tunnel tests using modal decomposition
AbstractSignal processing methods that remove noise due to atmospheric fluctuation and image sensors and extract fluid phenomena from schlieren...
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Density field reconstruction from time-series schlieren images via extended phase-consistent dynamic mode decomposition
The extended phase-consistent dynamic mode decomposition (DMD) method, which reconstructs density fields from density gradient fields in multiple...
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Machine learning-aided cooling profile prediction in plastic injection molding
This article discusses a new approach to develop a machine learning model for the cooling profile prediction of plastic parts produced through...
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Design Procedure of a Variable Rectangular Inlet for TBCC Engine Considering Mass Flow Requirements
Ramjet or scramjet engines, high-speed air-breathing propulsion systems, can only be operated in supersonic and hypersonic regions. Therefore, ramjet...
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Unmanned Air Vehicles
Unmanned air vehicles (UAVs) have become increasingly important in both civil and military roles. UAVs depend totally on avionic systems in order to...
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Aircraft High Lift System Asymmetric Fault Response Characteristics Research
Among the failure modes of high-lift systems, the transmission line disconnect failure mode is one of the most significant failure modes. After a...
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Key Technologies and Processes for Traditional Packaging
Today, traditional packaging technologies still play important roles for most of the ICs, MEMS, and sensors due to the advantages of low cost, good...
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Lift Generation Effect in Aerodynamic Layouts with a Submerged Air Intake Device and an Upper Planing Step
AbstractThe paper shows the effect of direct lift generation by an electrical impeller propulsion system integrated into the airfoil in aerodynamic...
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Development of a Testing Device for Measuring the Functional Parameters of UAV Recovery Systems
In the context of the increasingly dynamic development of Unmanned Aerial Vehicles (UAVs) and the fields in which they are used, as well as by the...
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The Research Progress and Prospect of Key Technologies in the Interior Weapon Cabin
The loading mode of weapons has always been a key issue in the field of development of fighter aircraft. With the development of high mobility,...
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A Brief Overview on Past Research on Coandă Assisted STOL Transport Aircraft
The Coordinated Reserch Center SFB 880 aimed at develo** technologies that enable aircraft designs for use on short airfields in the vicinity of...