日本マイクログラビティ応用学会誌
Print ISSN : 0915-3616
TR-IA ロケット5号機による均一噴霧の生成およびその燃焼実験
佐藤 順一野村 浩司 荒井 義人川崎 晴彦佐藤 龍也依田 真一
著者情報
ジャーナル オープンアクセス

1997 年 14 巻 3 号 p. 265-

詳細
抄録
Experimental study on formation of a homogeneous spray and its ignition and combustion were carried out by using microgravity conditions produced by the fifth TR-IA rocket. Condensation method was applied to generate homogeneous sprays. Methanol and air were used as a fuel and ambient gas, respectively. Shadowgraphy, shearing interferometry and PIV were employed to observe behaviors of a flame and droplets. Experiments were performed three times in 6 minutes microgravity conditions. Since enough amount of fuel to make a saturated fuel vapor-air mixture was not charged into a combustion chamber, no spray was generated. However, it was observed that a flame kernel grew spherically up to about 14 mm diameter in very lean premixtures. Temporal variations of the temperature profile of a flame kernel were measured with the shearing interferometer. These detailed data on ignition of lean premixtures have never been obtained under normal gravity conditions.
著者関連情報
© 1997 日本マイクログラビティ応用学会
前の記事 次の記事
feedback
Top