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Proceedings Paper

Experiment on fuel injection in high-enthalpy flow
Author(s): Hideyuki Tanno; Tomoyuki Komuro; Kazuo Sato; Katsuhiro Itoh; Shuichi Ueda
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Paper Abstract

An experiment of inert gas injection into a high enthalpy hypersonic air flow is described. Gaseous helium at room temperature was injected transversely through four (phi) 1.5 mm circular sonic injectors at a spacing of 20 mm, which was located 28 mm downstream from a backward-facing step of 4 mm height. The experiment was carried out in the high enthalpy shock tunnel HIEST under the free stream test condition at Mach number of 6.5 and at the velocity of 4 km/s. The purpose of the experiment was to examine transient behavior of the helium jet mixing with the test air flow. Sequential Schlieren flow visualization with high-speed CCD camera of 1 (mu) sec exposure time have been used. Pitot pressure profile in the helium jet was measured at three stream-wise location. The measurements showed that the helium jet reached to the steady state in less than 2 msec, which was within HIEST test duration.

Paper Details

Date Published: 17 April 2001
PDF: 8 pages
Proc. SPIE 4183, 24th International Congress on High-Speed Photography and Photonics, (17 April 2001); doi: 10.1117/12.424254
Show Author Affiliations
Hideyuki Tanno, National Aerospace Lab. (Japan)
Tomoyuki Komuro, National Aerospace Lab. (Japan)
Kazuo Sato, National Aerospace Lab. (Japan)
Katsuhiro Itoh, National Aerospace Lab. (Japan)
Shuichi Ueda, National Aerospace Lab. (Japan)

Published in SPIE Proceedings Vol. 4183:
24th International Congress on High-Speed Photography and Photonics
Kazuyoshi Takayama; Tsutomo Saito; Harald Kleine; Eugene V. Timofeev, Editor(s)

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