Effect of Non-uniform Flow on the Ignition and Combustion in Scramjet Combustor

• Published in: Электронное моделирование
• Date: 2007
• ISSN: 0204-3572
• Main Authors: Prahlada, Govindarajulu, Reddy, D.N.
• Format: Article
• Language: English
• Published: Інститут проблем моделювання в енергетиці ім. Г.Є. Пухова НАН України 2007
• Subjects: Применение методов и средств моделирования
• Online Access: https://nasplib.isofts.kiev.ua/handle/123456789/101628
• Journal Title: Digital Library of Periodicals of National Academy of Sciences of Ukraine
• Cite this: 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.

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...