Validation of drag estimation on wing-fuselage configurations for a Navier-Stokes solver

Masahiro Kondo, Guowei Yang, Shigeru Obayashi

研究成果: Conference contribution

抄録

An implicit multiblock Navier-Stokes solver, which utilizes the LU-SGS implicit method and the HLLEW scheme, has been developed for numerical simulations on complex and realistic aerodynamic configurations. One-level halo cells are used to communicate data between abutting blocks. The resulting method is applied to the NAL supersonic transport (SST) model, ONERA Model M5 configuration and DLR-F4 configuration to compare with experimental data.

本文言語English
ホスト出版物のタイトル41st Aerospace Sciences Meeting and Exhibit
出版ステータスPublished - 2003 12 1
イベント41st Aerospace Sciences Meeting and Exhibit 2003 - Reno, NV, United States
継続期間: 2003 1 62003 1 9

出版物シリーズ

名前41st Aerospace Sciences Meeting and Exhibit

Other

Other41st Aerospace Sciences Meeting and Exhibit 2003
国/地域United States
CityReno, NV
Period03/1/603/1/9

ASJC Scopus subject areas

  • 宇宙惑星科学
  • 航空宇宙工学

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