Notice of Retraction: Numerical simulation method research for scramjet integration performance

Weijie Gong, Shuo Tang

Research output: Chapter in Book/Report/Conference proceedingChapterpeer-review

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.

Original languageEnglish
Title of host publicationProceedings - 2010 3rd IEEE International Conference on Computer Science and Information Technology, ICCSIT 2010
PublisherIEEE Computer Society
Pages265-269
Number of pages5
ISBN (Print)9781424455386
DOIs
StatePublished - 2010

Publication series

NameProceedings - 2010 3rd IEEE International Conference on Computer Science and Information Technology, ICCSIT 2010
Volume8

Keywords

  • Chemical reaction
  • Hypersonic vehicle
  • Integrated design
  • Numerical simulation

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