水ロケットにおける飛行最適条件の研究

  • 太田 貴之
    名古屋大学大学院工学研究科博士前期課程
  • 梅村 章
    名古屋大学大学院工学研究科航空宇宙工学専攻

書誌事項

タイトル別名
  • Parametric Study of Water Rocket for Optimum Flight.
  • ミズ ロケット ニ オケル ヒコウ サイテキ ジョウケン ノ ケンキュウ

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抄録

Parametric study is conducted to find the optimum condition of water rocket for long flight, provided that the tank volume is prescribed. The parameters considered in the present study are the initial air pressure, water volume fraction, empty rocket mass, launching angle and bottle diameter which significantly affect the flight performance of water rocket. First, we calculate the temporal changes in tank pressure, water and air issue speeds and thrust, on the basis of a simple physical model which has been experimentally validated. Then, this model is incorporated into the equation of motion to calculate the ballistic flight of water rocket with various parameter values. As a result, it is found that PET bottles in the market are one of the most suitable for use as the pressure tank of water rocket.

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