Results 31 to 40 of about 7,514 (171)

Micro‐Doppler effect removal in inverse synthetic aperture radar imaging based on UNet

open access: yesElectronics Letters, Volume 59, Issue 9, May 2023., 2023
The micro‐Doppler (m‐D) effect caused by the rotational parts of the targets influences the quality of inverse synthetic aperture radar (ISAR) imaging. In this letter, a novel deep network‐assisted method is proposed to reduce the m‐D effect in ISAR imaging.
Haobo Wang, Yingxi Liu, Lei Ni, Ying Luo
wiley   +1 more source

Investigation of Micro Gas Turbine Systems for High Speed Long Loiter Tactical Unmanned Air Systems

open access: yesAerospace, 2019
In this study, the on-going research into the improvement of micro-gas turbine propulsion system performance and the suitability for its application as propulsion systems for small tactical UAVs (<600 kg) is investigated.
James Large, Apostolos Pesyridis
doaj   +1 more source

Converting an automobile turbocharger into a micro gas turbine [PDF]

open access: yesE3S Web of Conferences, 2019
A low cost micro turbojet made by using an automobile turbocharger and other automobile components for research is presented in this paper. The machine comprises mainly of three main assemblies, the compressor & turbine assembly, the combustion chamber ...
Butt M Usman
doaj   +1 more source

Power Balance Strategies in Steady-State Simulation of the Micro Gas Turbine Engine by Component-Coupled 3D CFD Method

open access: yesAerospace, 2023
Currently, an increasing number of designers have begun to pay attention to a new paradigm for evaluating the performance with full engine 3-dimensional computational fluid dynamics (3D CFD) simulations.
Yibing Xu   +4 more
doaj   +1 more source

Modeling and Performance Simulation of a Micro Turbojet Engine Using Flownex [PDF]

open access: yesIndian Journal of Science and Technology, 2019
Objectives: The study presents the results of modelling and analysis of a micro turbojet engine that can develop thrust in the range of 4 kN, that is sufficient to propel small UAVs and Drones. The modelling and simulation is carried out in Flownex simulation environment which is a powerful one-dimensional tool commercially available to analyze the ...
Swati Chauhan, G. Jims John Wessley
openaire   +1 more source

Pembuatan Ignition System Pada Micro Turbojet Engine AERO–16

open access: yesJurnal Mahasiswa Dirgantara, 2022
Prinsip kerja mesin turbojet bergantung dari komponen utamanya. Komponen utama dari mesin turbojet yaitu kompresor, ruang bakar, turbin. Sebelumnya telah dilakukan pembuatan micro turbojet engine aero – 16 dimana masih ada kekurangan yang harus diperbaiki, salah satunya ignition system.
Indirwan Alex   +2 more
openaire   +1 more source

Extreme Learning Machine-Based Diagnostics for Component Degradation in a Microturbine

open access: yesEnergies, 2022
Micro turbojets are used for propelling radio-controlled aircraft, aerial targets, and personal air vehicles. When compared to full-scale engines, they are characterized by relatively low efficiency and durability.
Nicola Menga   +4 more
doaj   +1 more source

Prediction of jet engine parameters for control design using genetic programming

open access: yes, 2014
The simulation of a jet engine behavior is widely used in many different aspects of the engine development and maintenance. Achieving high quality jet engine control systems requires the iterative use of these simulations to virtually test the ...
Giovanna Martinez Arellano   +5 more
core   +1 more source

ISWO-LADRC: Improved Spider Wasp Optimization Algorithm-Based Rotational Speed Control for Micro-Aero-Engine

open access: yesAerospace
Rotational speed is a key performance parameter of aero-engines. As an indispensable parameter in control systems, rotational speed has received widespread attention.
Huigui Long   +3 more
doaj   +1 more source

Automated axial flow turbine design with performance prediction [PDF]

open access: yesJournal of Engineering Science and Military Technologies, 2018
This paper describes the automation of preliminary 3D aerothermodynamic design and analysis of a single-stage axial flow turbine driving the compressor of the micro turbojet engine Jet Cat p200 using an analytical method.
Nader Elqussas   +3 more
doaj   +1 more source

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