日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
レーザーパルスジェットのノズル形状と推進性能の数値解析
葛山 浩弘岡 靖朗小紫 公也荒川 義博
著者情報
ジャーナル フリー

2005 年 53 巻 616 号 p. 237-240

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抄録
The relationship between the momentum-coupling coefficient C and the nozzle cone-angle of laser pulse-jets is investigated using Computational Fluid Dynamics. Temporal variations of thrust and pressure fields inside and outside conical nozzles are obtained, and computed C is compared with measured one. As a result, the computation well reproduces the measured C and its decreasing tendency with the nozzle cone-angle. The reason of this tendency is explained in relation to two-dimensional flow characteristics in its air-refresh process. In addition, it is suggested that the laser pulse width should be short enough that the laser-heated region can be smaller than the optimum nozzle size.
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© 2005 The Japan Society for Aeronautical and Space Sciences
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