𝔖 Bobbio Scriptorium
✦   LIBER   ✦

Effects of hydrogen active cooling on scramjet engine performance

✍ Scribed by Y. Tsujikawa; G.B. Northam


Publisher
Elsevier Science
Year
1996
Tongue
English
Weight
400 KB
Volume
21
Category
Article
ISSN
0360-3199

No coin nor oath required. For personal study only.


πŸ“œ SIMILAR VOLUMES


Effect of cooling channel geometry on re
✍ W. Bao; J. Qin; W.X. Zhou; D.R. Yu πŸ“‚ Article πŸ“… 2010 πŸ› Elsevier Science 🌐 English βš– 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

The effect of cooled shield properties o
✍ I.S. Zhitomirsky; V.G. Romanenko; A.L. Yastrgembsky πŸ“‚ Article πŸ“… 1984 πŸ› Elsevier Science 🌐 English βš– 221 KB

The effect of the conductive heat transfer for a cooled shield and convective heat transfer from the shield to the cooling vapour upon the heat flow through a cryostat insulation is studied.

Effect of wind on performance of a dry-c
✍ A.F. du Preez; D.G. KrΓΆger πŸ“‚ Article πŸ“… 1993 πŸ› Elsevier Science 🌐 English βš– 528 KB

The influence of cross-winds on the performance of a natural draft dry-cooling tower is investigated by means of full scale measurements. By monitoring all the relevant independent variables, the results of these measurements allow direct comparison with the wind effect predicted by a numerical proc