93   Artículos

 
en línea
Daniele Granata, Alberto Savino and Alex Zanotti    
The present study aimed to investigate the capability of mid-fidelity aerodynamic solvers in performing a preliminary evaluation of the static and dynamic stability derivatives of aircraft configurations in their design phase. In this work, the mid-fidel... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Haotian Luo, Weijun Pan, Yidi Wang and Yuming Luo    
Today, aviation has grown significantly in importance. However, the challenge of flight delays has become increasingly severe due to the need for safe separation between aircraft to mitigate wake turbulence effects. The primary emphasis of this investiga... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Seong Hyun Hong, Young Jin Kim, Soo Hyung Park, Sung Nam Jung and Ki Ro Kim    
The air and structural loads of a 5-ton class light helicopter (LH) rotor in a 2.24 g pull-up maneuver are investigated using a coupling between the computational structural dynamics (CSD) and computational fluid dynamics (CFD) methods. The LH rotor is c... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Zhou Shen, Beimeng Hu, Guozhan Li and Hongjun Zhang    
The effects of the coolant pulsation and the plasma aerodynamic actuation (PAA) on the film cooling are herein explored via large eddy simulations. The electrohydrodynamic force derived from the PAA was solved through the phenomenological plasma model. T... 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

 
en línea
Zijie Li and Hao Wang    
A recently developed launching device called the gun?track launch system is affected by its constrained track, such that the form of the muzzle jet changes from the state of free development in the entire space to a constrained state, where this lends un... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Ye Yuan, Weihong Gong, Guojun Wang and Jun Wang    
Pitch motion is the key factor affecting the performance characteristics of centrifugal pumps on board ships and exacerbates hydraulic excitation to induce the unsteady vibration of pump units. A hydraulic test platform with swing motion is established t... ver más
Revista: Water    Formato: Electrónico

 
en línea
Rafel Roig, Xavier Sánchez-Botello, Berhanu Mulu, Carl-Maikel Högström and Xavier Escaler    
The growing installation of intermittent renewable energy sources is forcing hydraulic turbines to work more frequently at speed no load when dangerous vaneless space vortex structures and stochastic flow phenomena can occur. An experimental campaign has... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Wei Gao, Yishu Liu, Qifu Li and Bei Lu    
Using the unsteady vortex lattice method based on the potential flow theory, a rapid modeling approach is developed for the aerodynamic computation of multi-lifting surfaces. Multiple lifting surfaces with different geometric parameters and grid division... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Donglong Zhou, Jianlong Chang and Huawei Shan    
In the combustion chamber of scramjets, fuel jets interact with supersonic airflow in the form of a liquid jet in crossflow (LJIC). It is difficult to achieve adequate jet?crossflow mixing and the efficient combustion of fuel in an instant. Large eddy si... ver más
Revista: Aerospace    Formato: Electrónico

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