Numerical simulation of hypervelocity flow on hemisphere in T2 shock tunnel

Michiko Furudate*, Bok Jik Lee, Eunju Jeong, Ln Seuck Jeung

*Corresponding author for this work

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

Abstract

Numerical simulations are thoroughly carried out for the flows in the nozzle and the test section in the T2 shock tunnel facility. In order to solve the flow realistically, an unsteady, axisymmetric, and nonequilibrium flow solver is employed. The thermochemical states of the gas are described by a four-temperature model. Obtained temperatures are compared with the experimental data measured by Palma using a Planar Laser-Induced Fluorescence (PLIF) Imaging technique.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
Pages6931-6938
Number of pages8
Volume10
StatePublished - 2006
Externally publishedYes
Event44th AIAA Aerospace Sciences Meeting 2006 - Reno, NV, United States
Duration: Jan 9 2006Jan 12 2006

Other

Other44th AIAA Aerospace Sciences Meeting 2006
CountryUnited States
CityReno, NV
Period01/9/0601/12/06

ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

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