Experimental study on effects of fuselage configurations for RLV on aerodynamic characteristics

W. Morita, T. Yoneda, Shigeru Aso, Yasuhiro Tani, Y. Inatani

研究成果: 書籍/レポート タイプへの寄稿会議への寄与

11 被引用数 (Scopus)

抄録

An experimental study on the effects of fuselage configurations for Reusable Launch Vehicle (RLV) on aerodynamic characteristics has been conducted. In the experiments circular, square and triangle cross sections are selected for the fuselage models of RLV. Aerodynamic forces of those models are measured and flow fields around those models are visualized by smoke-wire technique and oil-flow method. In the present study, the fuselage model with triangle cross section shows the highest values of CLmax and (L/D)max.

本文言語英語
ホスト出版物のタイトル34th AIAA Fluid Dynamics Conference and Exhibit
出版ステータス出版済み - 2004
イベント34th AIAA Fluid Dynamics Conference and Exhibit 2004 - Portland, OR, 米国
継続期間: 6月 28 20047月 1 2004

その他

その他34th AIAA Fluid Dynamics Conference and Exhibit 2004
国/地域米国
CityPortland, OR
Period6/28/047/1/04

!!!All Science Journal Classification (ASJC) codes

  • 工学(その他)
  • 航空宇宙工学

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