12   Artículos

 
en línea
Zhanlin Feng, Kuanliang Wang and Honghui Teng    
This study numerically investigates the effects of diluent gas proportion, the overdrive factor, and throat width on the wave structure and thrust performance of a ram accelerator operating in super-detonative mode. For premixed gas of a high energy dens... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Jianxiu Qin and Dehua Zhu    
Two-dimensional oblique detonation waves (ODWs) induced by finite wedges in a stoichiometric hydrogen?air mixture have been investigated numerically based on reactive Euler equations with a detailed chemical reaction model. The main zone affected by the ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Zijian Zhang and Ziqi Jiang    
Detonation initiation is a prerequisite to normal operations of an oblique detonation engine (ODE), and initiation-assistant measures are imperative in cases of initiation failure that occur in a length-limited combustor under wide-range flight condition... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Fan Yang, Mingyue Lin, Zongmin Hu and Guilai Han    
This paper investigates the flowfield patterns and distributions of surface heat flux of the cantilevered injection system for oblique detonation engine inlets. Three-dimensional complex shock wave/boundary layer interaction and shock wave/shock wave int... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Zhongqi Luo, Hexia Huang, Huijun Tan, Gang Liang, Jinghao Lv, Yuwen Wu and Liugang Li    
In this paper, the transient flow simulation in an annular isolator under rotating feedback pressure perturbations simplified from the rotating denotation wave (RDW) is performed. The instantaneous flow characteristics and the self-similarity of the isol... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Chian Yan, Hong Hui Teng, Xiao Cheng Mi and Hoi Dick Ng    
High-fidelity numerical simulations using a Graphics Processing Unit (GPU)-based solver are performed to investigate oblique detonations induced by a two-dimensional, semi-infinite wedge using an idealized model with the reactive Euler equations coupled ... ver más
Revista: Aerospace    Formato: Electrónico

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