Computation of hypersonic radiating flowfield over a blunt body

Takeharu Sakai, Tomoko Tsuru, Keisuke Sawada

Research output: Contribution to conferencePaperpeer-review

Abstract

A numerical method for calculating a strongly radiating axisymmetric flow field is developed. Radiative heat flux is determined one-, two-, and three-dimensionally using a model developed earlier which combines Planck, Rosseland and Gray-gas models. The flow solution is obtained with a fully implicit time-marching method using a full block matrix inversion. The method is applied for calculating the environments of a blunt body flying up to the velocity of 16 km/s. The calculated results are compared with the experimental data conducted in a ballistic range. The results show the calculated radiative heat; flux values are lower than the measured value by a factor of about five. The possible reasons for these discrepancies are given.

Original languageEnglish
Publication statusPublished - 1999
Externally publishedYes
Event37th Aerospace Sciences Meeting and Exhibit, 1999 - Reno, United States
Duration: 1999 Jan 111999 Jan 14

Other

Other37th Aerospace Sciences Meeting and Exhibit, 1999
Country/TerritoryUnited States
CityReno
Period99/1/1199/1/14

ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

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