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Effect of recooling cycle on performance of hydrogen fueled scramjet

โœ Scribed by J. Qin; S.L. Zhang; W. Bao; L. Zhang; W.X. Zhou

Book ID
119262489
Publisher
Elsevier Science
Year
2012
Tongue
English
Weight
857 KB
Volume
37
Category
Article
ISSN
0360-3199

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๐Ÿ“œ SIMILAR VOLUMES

Effect of cooling channel geometry on re
Effect of cooling channel geometry on re-cooled cycle performance for hydrogen fueled scramjet
โœ W. Bao; J. Qin; W.X. Zhou; D.R. Yu ๐Ÿ“‚ Article ๐Ÿ“… 2010 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 950 KB

Developing fuel with higher heat sink is widely carried out to meet the cooling requirement for an airbreathing hypersonic vehicle. However, a Re-Cooled Cycle has been newly proposed for a regeneratively cooled scramjet to reduce the fuel flow for cooling. Fuel heat sink (cooling capacity) is repeat