日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
バリスティック・レンジによる極超音速流実験 (第1報)
画像観測及びその処理方法
張 新宇辺見 真佐宗 章弘藤原 俊隆
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1993 年 41 巻 469 号 p. 81-87

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In order to investigate the atomic/molecular radiation from hypersonic flowfields, a small plastic projectile weighing 0.4g is accelerated up to higher than 5km/s using a ballistic range. A spectral measurement is done when a projectile passes through the test section, emitting radiation from its strong shock layer: The spectrographic data are obtained in the wavelength range 330 to 650nm. To study the radiation emission with high time-resolution, a high-speed shutter system using an image intensifier and a pulse generator is set up, giving a spatial distribution of radiation intensity in the shock layer. Another measurement is also done, taking framing pictures of the projectile during its flight. For the purpose of convenience, a transformation from the photographic to numerical data is performed, using a digital data-processing system composed of a CCD camera and an image processor. The measured results indicate that such measurement systems can be used in the study of reentry problems in a laboratory environment, after improving of the ballistic range performance.

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© The Japan Society for Aeronautical and Space Sciences
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