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Second Law Analysis of an Experimental Micro Turbojet Engine

2018
Mini class gas turbine engines are today used for small UAVs, cogeneration applications, and hybrid electric vehicle applications. In this paper, exergetic assessment of an indigenous mini class gas turbine engine is investigated. This engine is classified as mini class gas turbine where it differs from similar class engines in two ways, including ...
Kahraman, C.   +3 more
openaire   +2 more sources

Implementing Supplemental Fuel System for Testing Sustainable Aviation Fuel on TKT-1 Micro Turbojet Engine

International Symposium on Applied Computational Intelligence and Informatics
Sustainable Aviation Fuel (SAF) research has been gaining a lot of focus in the past era, the proof of that increased focus can be found in the various articles and investigations that are in the pipeline dealing with this subject.
Mhd Bashar Al Kazzaz, K. Beneda
semanticscholar   +1 more source

Selection of engine type for Micro Air Vehicles. Turbojet or turboprop?

International Journal of Technology Transfer and Commercialisation, 2008
Interactive communication, airspace explorations, optical-electronic complexes for mini-satellites, planetary protection system devices, identification of heavenly bodies of "asteroid-comet danger" class, etc., this is just a short list of the currently emerging branches of science and engineering, in which challenges could be solved only given that ...
A. Soudarev, A. Suryaninov
openaire   +1 more source

Development of Airborne Test Environment for Micro Turbojet Engine - Part II: Remote Measurement System

2020 New Trends in Aviation Development (NTAD), 2020
Turbojets still have their role in aviation, mostly due to the advent of unmanned aerial vehicles. The main goal of this research is to develop a preliminary airborne test bed for a micro turbojet engine to accomplish performance measurements.
Khaoula Derbel, K. Beneda
semanticscholar   +1 more source

Full-Flow Simulation-Based Analysis and Experimental Validation of the Overall Performance of Micro-Turbojet Engine

Journal of Fluids Engineering
The overall performance of the micro-turbojet engine (MTE) is typically assessed through parametric modeling, methods of component series calculation (CSC), and prototype experiments.
Tianhe Zhang, Lihong Wu, Zheng Li
semanticscholar   +1 more source

Advanced Data Acquisition System for Alternative Fuels Micro Turbojet Engine Test Bench

2020 New Trends in Aviation Development (NTAD), 2020
As in commercial aviation, military aircraft typically use gas turbine engines for propulsion. Regardless of the actual output being thrust or shaft power, each type employs similar working process to produce high energy gasses.
K. Beneda, László Kavas, B. Varga
semanticscholar   +1 more source

Development of Airborne Test Environment for Micro Turbojet Engine- Part I: Powerplant and Airframe Integration

2020 New Trends in Aviation Development (NTAD), 2020
Turbojets still have their role in aviation, mostly due to the advent of unmanned aerial vehicles. The main goal of the present research is to develop a preliminary airborne test bed for a micro turbojet engine to accomplish performance measurements. The
Khaoula Derbel
semanticscholar   +1 more source

Design of Two-Degree-of-Freedom Turbofan-Power-Ratio Control System for Micro Turbojet Engine

International Symposium on Applied Machine Intelligence and Informatics, 2019
Control of gas turbine engines is a safety critical aspect of the industry, regardless of power turbines or aviation power plants. Moreover, modern turbine control systems implement additional features that allow efficient operation throughout the widest
K. Beneda, Khaoula Derbel
semanticscholar   +1 more source

Modeling of Micro Turbojet Engine

AIAA Propulsion and Energy 2019 Forum, 2019
Mahmoud M. Ashry   +2 more
openaire   +1 more source

Off-design analysis of centrifugal compressor of micro turbojet engine 400 N using computational fluid dynamics

MACHINE LEARNING AND INFORMATION PROCESSING: PROCEEDINGS OF ICMLIP 2023, 2023
F. Z. Altair   +3 more
semanticscholar   +1 more source

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