94   Artículos

 
en línea
Jiajia Pan and Hung Tao Shen    
A two-dimensional wave model coupled with ice dynamics is developed to evaluate ice effects on shallow water wave propagation on a beach and in a channel. The nonlinear Boussinesq equations with ice effects are derived and solved by the hybrid technique ... ver más
Revista: Water    Formato: Electrónico

 
en línea
Bo Yang, Hesen Yang, Ning Zhao, Hua Liang, Zhi Su and Dongsheng Zhang    
The double-wedge configuration is a typical characteristic shape of the rudder surface of high-speed aircraft. The impact of the shock wave/boundary layer interaction and the shock wave/shock wave interaction resulting from the double wedge on aircraft a... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Fangyou Yu, Zhanbiao Gao, Qifan Zhang, Lianjie Yue and Hao Chen    
Suppressing shock-induced flow separation has been a long-standing problem in the design of supersonic vehicles. To reduce the structural and design complexity of control devices, a passive control technique based on micro-serrations is proposed and its ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Lakshmi Narayana Phaneendra Peri, Antonella Ingenito and Paolo Teofilatto    
The goal of this paper is to investigate the aerodynamic and aerothermodynamic behavior of the Schiaparelli capsule after the deployment of a supersonic disk-gap-band (DGB) parachute during its re-entry phase into the Martian atmosphere. The novelty of t... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Jayson Craig Small and Liwei Zhang    
The performance of detonation engines depends on propellant injectors. This study investigates a fluidic-valve injector mounted to a detonation tube. The injector is equipped with a recessed cavity connecting to the fuel plenum. After verifying the theor... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Bo Yang, Hesen Yang, Chuanbiao Zhang, Ning Zhao, Hua Liang and Dongsheng Zhang    
Compression corner shock wave/boundary layer interaction (SWBLI) is a typical shock wave/boundary layer interaction (SWBLI) problem in supersonic/hypersonic flows. In previous studies, the separation flow is usually caused by a single shock wave. However... 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
John-Paul Mosele, Andreas Gross and John Slater    
Shock wave boundary layer interactions are common to both supersonic and hypersonic inlet flows. Wall-resolved implicit large-eddy simulations of a canonical Mach 2.5 axisymmetric shock wave boundary layer interaction experiment at Glenn Research Center ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Davide Di Pasquale and Simon Prince    
Since modern transport aircraft cruise at transonic speeds, shock buffet alleviation is one indispensable challenge that civil transport research needs to be addressed. Indeed, in the transonic flow regime shock-induced separation and transonic buffet co... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Mengge Wang, Ziyun Wang, Yue Zhang, Daishu Cheng, Huijun Tan, Kun Wang and Simin Gao    
A shock wave/boundary layer interaction (SWBLI) is a common phenomenon in supersonic inlet flow, which can significantly degrade the aerodynamic performance of the inlet by inducing boundary layer separation. To address this issue, in this paper, we prop... ver más
Revista: Aerospace    Formato: Electrónico

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