Results 111 to 120 of about 161 (133)
Some of the next articles are maybe not open access.
Modeling of Micro Turbojet Engine
AIAA Propulsion and Energy 2019 Forum, 2019Mahmoud M. Ashry +2 more
openaire +1 more source
Flow physics in a micro turbojet engine inter-shaft fuel supply system
Physics of FluidsInter-shaft fuel supply systems (ISFSSs) consisting of a shaft annulus and a fuel slinger are usually used in micro turbojet engines to pump the fuel to the combustor, aiming at reducing engine's size and weight. Differing from the configuration with stationary fuel pipework, the fast-rotating shaft in the annulus would induce significant drag ...
Zhixun Wang +4 more
openaire +1 more source
Test Simulation and Control Law Optimization of Micro-Turbojet Engines
2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE), 2023Zhen Liu +5 more
openaire +1 more source
Vibration Analysis of a Micro Turbojet Engine under Two Impeller Structural Faults
Proceedings of Global Power & Propulsion SocietyDisk fracture and locking nut loosening of centrifugal impeller leads to severe vibration of micro turbojet engines, posing significant threats to engine stability and safety. In order to identify the engine vibration characteristics induced by the above two faults in a practical micro aero-engine, vibration acceleration of the engine casing is ...
Zhiming Yang +6 more
openaire +1 more source
The Aeronautical Journal
AbstractIn this study, measurements and numerical analyses of the temperature distribution of exhaust gas passing through two types of mixers using a micro turbojet engine were performed to investigate the flow mixing performance based on the shape of the mixer, which mixes the bypass air and core air in a gas turbine turbofan engine.
C. Lee, S.M. Choi
openaire +1 more source
AbstractIn this study, measurements and numerical analyses of the temperature distribution of exhaust gas passing through two types of mixers using a micro turbojet engine were performed to investigate the flow mixing performance based on the shape of the mixer, which mixes the bypass air and core air in a gas turbine turbofan engine.
C. Lee, S.M. Choi
openaire +1 more source
Trends of Micro Turbojet Engines within Thrust Range up to 1,000N
The KSFM Journal of Fluid Machinery, 2020Dong-Ho Rhee +2 more
openaire +1 more source
Experimental and Numerical Studies on Lobed Ejector Exhaust System for Micro Turbojet Engine
Engineering Applications of Computational Fluid Mechanics, 2011Yong Shan, Jing-Zhou Zhang
exaly

