32   Artículos

 
en línea
Junqiang Shi, Ziyang Li, Jingcheng Gao, Dongjing Chen, Xiaotao Li, Ying Li, Jin Zhang and Xiangdong Kong    
The integrated design of the motor and axial piston pump eliminates the coupling structure, resulting in a compact and lightweight motor-pump structure. The challenge of motors overheating has always been a major concern. To address this issue, the hydra... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Zhaohui Yao, Yiwen Qi, Wen Bao and Tianhong Zhang    
A high-precision variable-thrust control method based on real-time measurement of pintle displacement and closed-loop feedback control is proposed to solve the technical problems of deep throttling variable-thrust regulation and control of pintle liquid ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Nurfathin Zahrolayali, Mohd Rashdan Saad, Azam Che Idris and Mohd Rosdzimin Abdul Rahman    
Utilization of a heat source to regulate the shock wave?boundary layer interaction (SWBLI) of hypersonic inlets during throttling was computationally investigated. A plug was installed at the intake isolator?s exit, which caused throttling. The location ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Anandu Bhadran, Joel George Manathara and P. A. Ramakrishna    
This article explores the throttling aspect of the hybrid rocket motor through experiments using a lab-scale motor. The lab-scale motor utilizes a wax-Al based fuel and compressed air as the oxidizer. The oxidizer flow rate was modulated using a PID cont... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Xuan Jin, Yang Yang, Xiaomei Cao and Jinshui Wu    
The variable-area pintle injector has unique geometry and spray characteristics compared to traditional coaxial injectors, and is advantageous for weight lightening and deep throttling of liquid rocket engines. To obtain an accurate prediction of the spr... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Michele Ferlauto, Andrea Ferrero, Matteo Marsicovetere and Roberto Marsilio    
Aerospike nozzles represent an interesting solution for Single-Stage-To-Orbit or clustered launchers owing to their self-adapting capability, which can lead to better performance compared to classical nozzles. Furthermore, they can provide thrust vectori... ver más

 
en línea
Won Cho and Joonho Kong    
In this paper, we introduce a memory and cache contention denial-of-service attack and its hardware-based countermeasure. Our attack can significantly degrade the performance of the benign programs by hindering the shared resource accesses of the benign ... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Tim Wittmann, Sebastian Lück, Christoph Bode and Jens Friedrichs    
Radial turbines used in automotive fuel cell turbochargers operate with humid air. The gas expansion in the turbine causes droplets to form, which then grow through condensation. The associated release of latent heat and decrease in the gaseous mass flow... ver más

 
en línea
Vladimir Kodnyanko, Stanislav Shatokhin, Andrey Kurzakov, Yuri Pikalov, Iakov Pikalov, Olga Grigorieva, Lilia Strok and Maxim Brungardt    
Aerostatic bearings are attractive, with minimal friction losses, high durability, and environmental friendliness. However, such designs have a number of disadvantages, including low load-bearing capacity and high compliance due to high air compressibili... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Victor Goman, Vladimir Prakht, Vadim Kazakbaev and Vladimir Dmitrievskii    
The presented results can be used to evaluate the energy-saving potential and ecological impact of electric motors of various energy efficiency classes in various applications of electric drive.
Revista: Applied Sciences    Formato: Electrónico

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