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Comprehensive approach to static firing tests of micro gas turbine engines powered by liquid fuels
DV Antonov, RE Cherkasov, VV Gneusheva… - Energy, 2024 - Elsevier
The paper presents test results on the combustion of liquid fuels in micro gas turbine
engines (MGTE). A setup was designed and built to determine the following MGTE …
engines (MGTE). A setup was designed and built to determine the following MGTE …
[HTML][HTML] Optimization for aerodynamic performance of double serpentine nozzles with spanwise offsets using Taguchi-based CFD analysis
X Zhang, S Yong, J Zhang, WU Zhongcheng - Chinese Journal of …, 2023 - Elsevier
Serpentine nozzles are widely used in combat aircraft to realize strong stealth
characteristics. Based on the layout characteristics within a confined space, a series of …
characteristics. Based on the layout characteristics within a confined space, a series of …
Assessment of fan stall point identification ability of steady RANS computations with the helicity-corrected Spalart-Allmaras turbulence model
Z Yu, H Raza, J Defoe - Turbo Expo: Power for Land …, 2023 - asmedigitalcollection.asme.org
Accurate axial fan/compressor stall point prediction using computational fluid dynamics
(CFD) has generally been carried out using unsteady computations, often with slowly …
(CFD) has generally been carried out using unsteady computations, often with slowly …
Research on the failure mechanism in the convergent section of an aero-engine's adjustable nozzle under multi-field coupling analyses
H Miao, C Li, L Lao, J Hong, Y Ma - Engineering Failure Analysis, 2025 - Elsevier
Heat shields are critical yet vulnerable components that widely utilized in the exhaust
nozzles of aero-engines to safeguard the relevant structures against the exhaust gas in …
nozzles of aero-engines to safeguard the relevant structures against the exhaust gas in …
Numerical analyses on the feasibility of TC type nozzles in ocean thermal energy Conversion turbines
Q Ma, J Huang, H Lu, H Luo, J Li, Z Wu… - Energy Sources, Part A …, 2024 - Taylor & Francis
The turbine is a crucial component in harnessing ocean thermal energy (OTE), and the
impact of the nozzle on turbine performance is significant. TC-profile nozzles have been …
impact of the nozzle on turbine performance is significant. TC-profile nozzles have been …
Turbojet thrust augmentation through a variable exhaust nozzle with active disturbance rejection control
Turbojets require variable exhaust nozzles to fit high-demanding applications; however, few
reports on nozzle control are available. The purpose of this paper is to investigate the …
reports on nozzle control are available. The purpose of this paper is to investigate the …
Applicability of correlational data-mining to small-scale turbojet performance map generation
F Villarreal-Valderrama, P Juárez-Pérez… - International Journal of …, 2024 - degruyter.com
Turbojet applications benefit from accurate performance models. The aim of this study is to
explore the applicability of data-mining algorithms to determine relationships between the …
explore the applicability of data-mining algorithms to determine relationships between the …
A novel non-embedded, adjustable, and flexible shape memory alloy actuator for variable-area exhaust nozzle actuation
T Chen, Y Ke, S Qiu, J Jiang, Q Zhang… - Review of Scientific …, 2023 - pubs.aip.org
The actuator is a fundamental component for a variable-area exhaust nozzle. Conventional
actuators for variable-area exhaust nozzles are hydraulic actuators and electric motors …
actuators for variable-area exhaust nozzles are hydraulic actuators and electric motors …
Study on combustion and emission characteristics of a micro‐rotary cam internal combustion engine
H Zhu, M Yang, H Hao, L Chen - Engineering Reports, 2024 - Wiley Online Library
In this article, the construction principle of rotary engine and sliding vane internal
combustion engine is carefully analyzed, and the concept of micro‐rotary cam internal …
combustion engine is carefully analyzed, and the concept of micro‐rotary cam internal …
Modeling and controller design of vertical take-off and landing turbojet powered aircraft
T Ouyang, Y Yin, F Kang, J Zhang… - 2024 7th …, 2024 - ieeexplore.ieee.org
Aiming at the problems such as high altitude flight difficulty and poor wind resistance of
rotary-wing UAV in disaster rescue, this paper proposes a vertical take-off and landing …
rotary-wing UAV in disaster rescue, this paper proposes a vertical take-off and landing …