284   Artículos

 
en línea
Yihe He, Xiaojuan Shi and Honghu Ji    
Based on the orthogonal experimental method, a simulation case of the flow field of the ejector nozzle was designed to investigate the influence of the structural parameters of the ejector nozzle on the internal and external flow. This study explored the... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yingke Liao, Guiping Zhu, Guang Wang, Jie Wang and Yanchao Ding    
Magnetohydrodynamic (MHD) is one of the most promising novel propulsion technologies with the advantages of no pollution, high specific impulse, and high acceleration efficiency. As the carrier of this technology, the MHD accelerator has enormous potenti... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Murat Millidere, Ferhat Akgül, Kemal Leblebicioglu and James F. Whidborne    
For developing high-fidelity flight simulations, an accurate and complete representation of the aerodynamic characteristics of the aircraft is necessary. To obtain a realistic aerodynamic database, system identification methods can be used to describe th... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Zhiyuan Hu, Peng Yu, Guohua Xu, Yongjie Shi, Feng Gu and Aijun Zou    
Tiltrotors permit aircrafts to operate vertically with lift, yet convert to ordinary forward flight with thrust. The challenge is to design a tiltrotor blade yielding maximum lift and thrust that converts smoothly without losing integrity or efficiency. ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Jason Cornelius, Sven Schmitz, Jose Palacios, Bernadine Juliano and Richard Heisler    
This work details the development and validation of a methodology for high-resolution rotor models used in hybrid Blade Element Momentum Theory Unsteady Reynolds Averaged Navier?Stokes (BEMT-URANS) CFD. The methodology is shown to accurately predict sing... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Shuli Wang, Ziang Li and Qingxin Zhang    
The electric seaplane, designed for take-off and landing directly on water, incorporates additional structures such as floats to meet operational requirements. Consequently, during the take-off taxiing phase, it encounters significantly higher aerodynami... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Luisa Boni, Marco Bassetto and Alessandro A. Quarta    
Photonic solar sails are a class of advanced propellantless propulsion systems that use thin, large, lightweight membranes to convert the momentum of light from the Sun into thrust for space navigation. The conceptually simple nature of such a fascinatin... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Dongfeng Yan, Zehang Zhao, Anchen Song, Fengming Li, Lu Ye, Ganchao Zhao and Shan Ma    
The fluidic pintle nozzle, a new method to control the thrust of a solid rocket motor, has been proposed in recent years by combining the pintle with the aerodynamic throat (fluidic throat). The study of static characteristics has proved that it has a re... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Saroj Maharjan, Antoine Poujol, Christophe Martin, Gabriele Ameri, David Baumont, Kiana Hashemi, Yacine Benjelloun and Hussein Shible    
Nepal is one of the most seismically active regions in the world, as highlighted by the recent devastating 2015, Mw~7.8 Gorkha earthquake, and a robust assessment of seismic hazard is paramount for the design of earthquake-resistant structures. In this s... ver más
Revista: Geosciences    Formato: Electrónico

 
en línea
Hung-Ta Wen, Hom-Yu Wu, Kuo-Chien Liao and Wei-Chuan Chen    
In recent years, artificial intelligence (AI) technology has been applied in different research fields. In this study, the XGBoost regression model is proposed to estimate JT9D engine thrust. The model performance mean absolute error (MAE) is 0.004845, t... ver más
Revista: Aerospace    Formato: Electrónico

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