Research on quasi one dimensional modeling of the scramjet engine

Dong Zhang, Shuo Tang, Qiang Jun Zhu

Research output: Contribution to journalArticlepeer-review

6 Scopus citations

Abstract

The quasi one dimensional flow field analysis model for the scramjet engine was built based on the theory of quasi one dimensional flow and the influence coefficient method. Some influence factors were considered in the model, such as the quality of fuel additive, the changes of section, the wall friction and the chemical heat release. The parameters variations along the axis direction and the exit parameters of the scramjet can be given in a short time by using the analysis model. Focused on an airframe/propulsion integrated single module vehicle, the accuracy of the quasi one dimensional model was verified through comparison with the CFD. The results show that the quasi one dimensional model is simple, rapid, and highly accurate for calculation and analysis for the scramjet, and can be used in the preliminary stage.

Original languageEnglish
Pages (from-to)192-197
Number of pages6
JournalGuti Huojian Jishu/Journal of Solid Rocket Technology
Volume38
Issue number2
DOIs
StatePublished - 1 Apr 2015

Keywords

  • Air-breathing hypersonic vehicle
  • Influence coefficient method
  • Quasi one dimensional model
  • The scramjet engine

Fingerprint

Dive into the research topics of 'Research on quasi one dimensional modeling of the scramjet engine'. Together they form a unique fingerprint.

Cite this