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: 著書/レポートタイプへの貢献会議での発言

11 引用 (Scopus)

抜粋

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.

元の言語英語
ホスト出版物のタイトル34th AIAA Fluid Dynamics Conference and Exhibit
出版物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 28 20047 1 2004

その他

その他34th AIAA Fluid Dynamics Conference and Exhibit 2004
米国
Portland, OR
期間6/28/047/1/04

    フィンガープリント

All Science Journal Classification (ASJC) codes

  • Engineering (miscellaneous)
  • Aerospace Engineering

これを引用

Morita, W., Yoneda, T., Aso, S., Tani, Y., & Inatani, Y. (2004). Experimental study on effects of fuselage configurations for RLV on aerodynamic characteristics. : 34th AIAA Fluid Dynamics Conference and Exhibit