Effect of Non-uniform Flow on the Ignition and Combustion in Scramjet Combustor
The uniform and nonuniform flow conditions are created at the entry of the combustor by incorporating a Circle to Rectangle Transition duct (CR-Transition duct, for short) in the subsonic and supersonic flows ahead of the combustor. Computational and experimental studies have been carried out on a r...
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| Veröffentlicht in: | Электронное моделирование |
|---|---|
| Datum: | 2007 |
| Hauptverfasser: | , , |
| Format: | Artikel |
| Sprache: | Englisch |
| Veröffentlicht: |
Інститут проблем моделювання в енергетиці ім. Г.Є. Пухова НАН України
2007
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| Schlagworte: | |
| Online Zugang: | https://nasplib.isofts.kiev.ua/handle/123456789/101628 |
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| Назва журналу: | Digital Library of Periodicals of National Academy of Sciences of Ukraine |
| Zitieren: | Effect of Non-uniform Flow on the Ignition and Combustion in Scramjet Combustor / Prahlada, Govindarajulu, D.N. Reddy // Электронное моделирование. — 2007. — Т. 29, № 1. — С. 97-105. — Бібліогр.: 17 назв. — англ. |