Numerical simulation of the integrated space shuttle vehicle in ascent

P. G. Buning, I. T. Chiu, S. Obayashi, Y. M. Rizk, J. L. Steger

研究成果: Paper査読

32 被引用数 (Scopus)

抄録

A simulation of the flow about the integrated space shuttle vehicle in ascent mode has been undertaken for various flight conditions using the Chimera composite grid discretization approach. Overset body-conforming grids were used to represent each geometric component, and an implicit approximately factored finite-difference procedure was used to solve the three-dimensional thin-layer Navier-Stokes equations. The computational results have been compared with both wind tunnel and flight test data. Although relatively good agreement is obtained with the experimental data, further refinement and evaluation of numerical error is under way.

本文言語English
ページ265-283
ページ数19
DOI
出版ステータスPublished - 1988
外部発表はい
イベント15th Atmospheric Flight Mechanics Conference, 1988 - Minneapolis, United States
継続期間: 1988 8 151988 8 17

Other

Other15th Atmospheric Flight Mechanics Conference, 1988
CountryUnited States
CityMinneapolis
Period88/8/1588/8/17

ASJC Scopus subject areas

  • Mechanical Engineering
  • Aerospace Engineering

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