Reduction of aerodynamic interference for separation of two-stage reusable launch vehicles

Taro Uematsu, Takuro Ishida, Shigeru Aso, Yasuhiro Tani

研究成果: 書籍/レポート タイプへの寄稿会議への寄与

6 被引用数 (Scopus)

抄録

In this paper, we focused on reduction of reflected shock wave generated between two bodies in hypersonic flow field. Problem of the flow field was modeled as flow field between the flat plate with wedge-shaped at the top and slender body in hypersonic flow field. The slender body has three cross section configuration patterns (circle, triangle and square). We carried out 3-D numerical calculation for the modeled flow field and conducted wind tunnel experiment. From their results, the slender body having triangle cross section can reduce the reflected shock wave.

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 - 12月 1 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

フィンガープリント

「Reduction of aerodynamic interference for separation of two-stage reusable launch vehicles」の研究トピックを掘り下げます。これらがまとまってユニークなフィンガープリントを構成します。

引用スタイル