TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
Online ISSN : 1884-0485
ISSN-L : 1884-0485
a) Chemical Propulsion and Air-breathing Engines
Induction Phenomena of Laser Ignition
Nao AKASHIYoshihiro HARAKeisuke KONDOHideyuki HORISAWA
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2014 Volume 12 Issue ists29 Pages Pa_79-Pa_84

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Abstract

A preliminary study on induction phenomena of laser-ignition was conducted. For observation of the initial phenomena, an experimental study on effects of a focused laser pulse (Nd:YAG, 335mJ/pulse, pulse width 5nsec) into a hydrogen-air mixture was conducted. Temporal evolutions of typical line spectra of a laser-induced plasma of the mixture were measured with the photodiode through specific band-pass filters for each spectrum for N+, H, and O, and also with a time-resolved ICCD spectroscopic analyzer. As the results, it was found that phenomena occurring after laser irradiation up to combustion completion were divided into three processes; i) absorption process of an incident laser pulse (2 x 10-9~ 10-8 sec), ii) plasma formation process (ionic emission by 400 nsec followed by atomic emission) (10-8 ~ 10-6 sec), and iii) ignition (10-5 ~ 10-4 sec), having various scales of the characteristic times. In addition, temporal evolution of electronic excitation temperature of N+ ions was estimated from the Boltzmann plots. It was shown that the temperature was about 25,000 K at initial 200 ~ 400 nsec, and then gradually decreased 20,000 K at 900 nsec. Moreover, electron densities were also estimated from the Stark broadening widths of Hα and Hβ spectra. Temporal evolution of the electron density showed the electron density of about 4 x 1017 cm-3 at initial 300 nsec, and then, down to 1.3 x 1017 cm-3 at 900 nsec.

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© 2014 The Japan Society for Aeronautical and Space Sciences
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