Results 21 to 30 of about 512 (187)
The combustor exit temperature distribution of an aero-engine is a key factor affecting the thermal load and service life of turbine blades. To address the thermal fatigue of the blade shroud, tip, and root caused by local overheating at the outlet of a ...
Zhenpeng He +9 more
doaj +1 more source
The aerothermal interaction of the combustor exit flow on the first vane row has been examined at the Large Scale Turbine Rig (LSTR) at Technische Universität Darmstadt (Darmstadt, Germany).
Holger Werschnik +5 more
doaj +1 more source
The liner temperature distribution of an aero-engine combustor is a critical parameter for evaluating its cooling effectiveness. It provides essential guidance for designing the combustor cooling flow field, assessing combustion performance, identifying ...
Yu Huang +7 more
doaj +1 more source
Control Oriented Model for Expander Cycle Scramjet
As a efficient and simple design, expander cycle is widely applied in LRE engineering, but it is seldomly used on scramjet research. In order to establish a complete mathematical model for expander cycle scramjet, a control-oriented model for expander ...
Zhao Zhelong, Wu Xianyu
doaj +1 more source
Effect of Cooling Air on Swirl Combustor
This paper presents the numerical study of the turbulent swirling flow in a combustor and the effect of cooling air, which has practical applications in industrial furnaces and jet engines. Cooling air is used to protect the combustor wall from burnout, while allowing the combustion to occur at higher temperature.
Md. Shiblee Noman +1 more
openaire +2 more sources
This study presents a novel 3‐reactor chemical looping system for CO2 capture and subsequent utilization with biomass and natural gas for producing liquid fuels. Using Ca2Fe2O5\Fe2O3 oxygen carriers, it achieves 60% CO2 capture efficiency, ∼80% syngas purity, and autothermal operation, offering a scalable, carbon‐negative route to sustainable fuels ...
Krutarth Pandit +6 more
wiley +1 more source
Research on optimization of combustor liner structure based on arc-shaped slot hole
The flow and heat transfer characteristics of the fluid in the combustor were investigated using numerical simulation in this study. The physical properties of the cooling airflow were fully utilized, and the structure of the combustor was improved. Film
He Zhenpeng +6 more
doaj +1 more source
Evaluation of machine learning models for predicting performance metrics of aero-engine combustors
As environmental standards tighten and aero-engine performance improves, credible mapping between structural parameters and performance metrics is crucial for optimizing combustion chamber design.
Huan Yang +4 more
doaj +1 more source
A first‐of‐its‐kind review benchmarks three solar methane valorization pathways with unified performance metrics for clean fuel production. Meeting global climate targets and sustainable energy demands requires carbon‐neutral fuels and innovative conversion pathways.
Muhammad Abdulmoez +3 more
wiley +1 more source
With the increasing power output of aero-engines, combustor hot-gas mass flow rate and temperature continue to rise, posing more severe challenges to combustor structural cooling design. To enhance the film-cooling performance of the Z-profile feature in
Jiaxiao Yi +3 more
doaj +1 more source

