๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Heat transfer characteristics of spray cooling in a closed loop

โœ Scribed by Lanchao Lin; Rengasamy Ponnappan


Publisher
Elsevier Science
Year
2003
Tongue
English
Weight
320 KB
Volume
46
Category
Article
ISSN
0017-9310

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


Heat transfer characteristics of a reser
โœ Hiroaki Ishikawa; Tetsuro Ogushi; Takehide Nomura; Hiroyuki Noda; Haruo Kawasaki ๐Ÿ“‚ Article ๐Ÿ“… 2007 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 786 KB

## Abstract Highโ€powered satellites need larger heat rejection areas. A deployable radiator is one of the key technologies for a highโ€powered satellite bus. A Reservoir Embedded Loop Heat Pipe (RELHP) is a twoโ€phase heat transfer device that constitutes the deployable radiator. RELHP has an evapora

Heat transfer characteristics in a conde
โœ Hiroyuki Hashimoto; Fumito Kaminaga ๐Ÿ“‚ Article ๐Ÿ“… 2002 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 165 KB

## Abstract Condensation heat transfer in a closed twoโ€phase thermosyphon is experimentally examined using two different types of test section. Test Section 1 is a straightโ€pipeโ€type thermosyphon, whereas Test Section 2 has a largeโ€diameter evaporator compared with a condenser to minimize entrainme

Flow and heat transfer characteristics i
โœ J. Qin; W. Bao; W.X. Zhou; D.R. Yu ๐Ÿ“‚ Article ๐Ÿ“… 2010 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 865 KB

Developing fuel with higher heat sink is widely carried out to meet the cooling requirement for an air breathing hypersonic vehicle. Especially, a recooling cycle has been newly proposed for an actively cooled scramjet to reduce the fuel flow for cooling. Fuel heat sink (cooling capacity) is repeate