@inbook{b9a9864ef95b41b0a14bacde07e5fe4a,
title = "Notice of Retraction: Numerical simulation method research for scramjet integration performance",
abstract = "Scramjet technology is one of the key technologies of hypersonic vehicle design powered by air-breathing engine, and its work progress is extremely complicated. In order to explore the scramjet working condition and the operation mechanism, the Scramjet Integration Performance is calculated by Numerical Simulation Method which adopts the two-dimensional NS equation, explicit MacCormack format. The inside flow field of scramjet is analyzed to different mach numbers. and for the complex chemical reactions of the combustor, a hydrogen-oxygen chemical reaction model is created to analyze the baseline model chemical reactions of the combustor, and the reasonable proposals are presented for the baseline model.",
keywords = "Chemical reaction, Hypersonic vehicle, Integrated design, Numerical simulation",
author = "Weijie Gong and Shuo Tang",
year = "2010",
doi = "10.1109/ICCSIT.2010.5564606",
language = "英语",
isbn = "9781424455386",
series = "Proceedings - 2010 3rd IEEE International Conference on Computer Science and Information Technology, ICCSIT 2010",
publisher = "IEEE Computer Society",
pages = "265--269",
booktitle = "Proceedings - 2010 3rd IEEE International Conference on Computer Science and Information Technology, ICCSIT 2010",
}