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
β¦ LIBER β¦
Effects of hydrogen active cooling on scramjet engine performance
β Scribed by Y. Tsujikawa; G.B. Northam
- Publisher
- Elsevier Science
- Year
- 1996
- Tongue
- English
- Weight
- 400 KB
- Volume
- 21
- Category
- Article
- ISSN
- 0360-3199
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