Results 11 to 20 of about 4,282 (226)
Recent Advancements in Design Optimization of Lattice‐Structured Materials
Enhancement in the performance of lattice materials involves improving the design in the manufacturing process. Functional gradation and multimorphology strategies are utilized to enhance the multifunctionality of lattice materials. As the preceding strategies involve challenges and limitations, utilizing them concurrently with automated design ...
Abdulla Alhembar +4 more
wiley +1 more source
In order to rapidly predict the performance of hydrocarbon-fueled regeneratively cooled scramjet engine in system design, a quasi-one-dimensional model has been developed.
Yuefei Xiong +4 more
doaj +1 more source
A reliable combustion monitoring system is essential to satisfy global carbon neutrality trends. As the concentrations of emissions and flame stability are associated with the air–fuel ratio, the equivalence ratio should be continuously evaluated. In this study, a deep neural network‐ (DNN‐) based regression model is proposed to predict the equivalence
Sanghun Shin +4 more
wiley +1 more source
Summary of Active Mixing Enhancement Technology for Scramjet [PDF]
Fuel mixing and enhancement is the key technology of modern scramjet engine. In view of the problem of how to fully mix fuel, researchers have developed a variety of mixing enhancement technologies, which are mainly divided into active and passive types.
Wang Wenlong, Gai Zilin, Ma Cenrui, Wang Hongyu
doaj +1 more source
Review on Creep Phenomenon and Its Model in Aircraft Engines
The aircraft is subjected to high‐temperature and high‐pressure conditions during flight, which renders it susceptible to the occurrence of creep phenomenon. Several academics have conducted extensive research on this issue. This research paper provides a comprehensive overview of the existing literature on creep phenomena in aircraft engines.
Lin Yuan +7 more
wiley +1 more source
Comparison of Dual-Combustion Ramjet and Scramjet Performances Considering Combustion Efficiency
The performances of a dual-combustion ramjet (DCR) and a scramjet were compared via computational fluid dynamics numerical simulation to provide theoretical guidance for engine selection for a hypersonic vehicle.
Xianju Wu, Zhijun Wei
doaj +1 more source
The objective of this paper is to numerically study the shock wave/boundary layer interaction and boundary layer separation. The first stage of this research is the development of methodology, flow simulations, and data analysis. When comparing the plots, it can be seen that the results of the check of the methodology were similar.
Ana Maria Pereira Lara +2 more
wiley +1 more source
A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor
In this work, a new configuration of strut-based scramjet is proposed, and a series of simulations are conducted to investigate its possibility of practical application.
Linqing Zhang +4 more
doaj +1 more source
Liquid oxygen chill‐down in a straight horizontal pipe was studied experimentally. The effect of the entrance corner was excluded, and much denser wall temperature sensors along the pipe have been set compared to the present studies. In this way, the chill‐down process, as well as the development of the flow pattern, has been drawn for every test. As a
Lanwei Chen, Jiaqi Zhang, Yiheng Tong
wiley +1 more source
Bleeding is an effective method to improve the starting performance of the inlet, and the conventional method often adopts the bleeding to longitudinal direction. This article proposes the use of transversal bleeding method to explore the influence on starting capacity by changing the bleeding direction. The paper designs 6 bleeding inlets.
Tianyu Gong +5 more
wiley +1 more source

