A study of fuselage configurations for reusable launch vehicles

Takuro Ishida, Shigeru Aso, Yasuhiro Tani, Yoshifumi Inatani, Tomoko Irikado

研究成果: 書籍/レポート タイプへの寄稿会議への寄与

5 被引用数 (Scopus)

抄録

A numerical study on the fuselage configurations of reusable launch vehicles (RLVs) has been conducted. The models for the numerical simulations were the models which wind tunnel experiments were conducted previously (named in this paper as triangle and square) and a new proposal one which modified the cross sectional configuration. (named as modified triangle) The results from triangle and square models showed that in supersonic region, the formations of separated vortex on the fuselage surfaces are quite different from subsonic case. With the results from modified triangle model, it is obvious that changing the separation lines has the effect to enlarge the region which separated vortex develops.

本文言語英語
ホスト出版物のタイトル47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
出版ステータス出版済み - 2009
イベント47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition - Orlando, FL, 米国
継続期間: 1月 5 20091月 8 2009

出版物シリーズ

名前47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

その他

その他47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
国/地域米国
CityOrlando, FL
Period1/5/091/8/09

!!!All Science Journal Classification (ASJC) codes

  • 宇宙惑星科学
  • 航空宇宙工学

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