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Numerical simulation study of aerodynamic characteristic on hypersonic aircraft

  • Jiang Chen*
  • , Song Ping Wu
  • *Corresponding author for this work
  • Beihang University

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

In this paper, a three dimension model that is similar to the hypersonic cruise aircraft X-51A has been generated by using a graphics processing technology and an anti-modeling method from the published pictures and related articles about the X-51A. This paper adopts the Harten-Yee's scheme to simulate the aircraft at the cruise state of M∞=6, α=6°. And related results are acquired. Analyze the basic characteristics of the flow-field qualitatively and find that the result is kept well with the designed state. So it means that the model could be used for the further related research.

Original languageEnglish
Title of host publicationProceedings of the 2012 National Conference on Information Technology and Computer Science, CITCS 2012
Pages341-343
Number of pages3
StatePublished - 2012
Event2012 National Conference on Information Technology and Computer Science, CITCS 2012 - Lanzhou, China
Duration: 16 Nov 201218 Nov 2012

Publication series

NameProceedings of the 2012 National Conference on Information Technology and Computer Science, CITCS 2012

Conference

Conference2012 National Conference on Information Technology and Computer Science, CITCS 2012
Country/TerritoryChina
CityLanzhou
Period16/11/1218/11/12

Keywords

  • Aerodynamic characteristic
  • Hypersonic
  • Numerical simulation

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