6   Artículos

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en línea
Balázs Both, Zoltán Szánthó     Pág. 129 - 136
In this paper an offset, attached jet is investigated both experimentally and numerically, applying the tangential room air distribution system. The attachment distance of the injected air jet, which influences the ventilation characteristics in the room... ver más
Revista: Periodica Polytechnica: Mechanical Engineering    Formato: Electrónico

 
en línea
Yuyang Liu and Xian Yi    
The tangential jet-induced swirling flow is a highly efficient technology for enhancing heat transfer. This paper explores the application of swirling flow of an airfoil/aero-engine in a hot air anti-icing chamber, aiming to improve the anti-icing perfor... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Svitlana Khadzhynova     Pág. 47 - 54
It has been proposed to modify the surface of offset and coated paper with a special coating (primer) that ensures the high quality of ink-jet printing, specifically barcodes. The application of digital ink-jet printing using aqueous-based inks makes it ... ver más
Revista: Eastern-European Journal of Enterprise Technologies    Formato: Electrónico

 
en línea
Andrea M. Gomez, Kyle C. McDonald, Karsten Shein, Stephanie DeVries, Roy A. Armstrong, William J. Hernandez and Milton Carlo    
Coral reefs are among the most biologically diverse ecosystems on Earth. In the last few decades, a combination of stressors has produced significant declines in reef expanse, with declining reef health attributed largely to thermal stresses. We investig... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Pooneh Aref, Mehdi Ghoreyshi, Adam Jirasek and Matthew J. Satchell    
The flow physics modeling and validation of the Royal Aircraft Establishment (RAE) subsonic intake Model 2129 (M2129) are presented. This intake has an 18 inches long S duct with a 5.4 inches offset, an external and an internal lip, forward and rear exte... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Pooneh Aref, Mehdi Ghoreyshi, Adam Jirasek and Matthew J. Satchell    
The flow physics modeling and validation of the Royal Aircraft Establishment (RAE) subsonic intake Model 2129 (M2129) are presented. This intake has an 18 inches long S duct with a 5.4 inches offset, an external and an internal lip, forward and rear exte... ver más
Revista: Aerospace    Formato: Electrónico

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