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  • 荻須 吉洋
    燃料協会誌
    1981年 60 巻 2 号 121-127
    発行日: 1981/02/20
    公開日: 2010/06/28
    ジャーナル フリー
    As an example of practical combustors, the pot type burner and the premixed gas burner were studied.The relations between the level and the spectrum or combustion noise from these types of combustor and the condition of combustion were studied experimentally, and three suggestions for the low noise burner were shown as follows.
    1) to burn in premixed
    2) to use smaller and many ports, distributed in three-dimentional position
    3) to use strong flame holding system (As the bluff body causes excessive turbulence, pilot burner type flame holding is favourable.)
  • 速度分布に及ぼす影響
    木村 一郎, 米持 政忠
    計測自動制御学会論文集
    1978年 14 巻 2 号 196-201
    発行日: 1978/04/30
    公開日: 2009/03/27
    ジャーナル フリー
    The effects of sound on air jets have been studied by many researchers, but the behaviour of two-dimensional water jets sensitive to sound, which is especially important for the application of fluidics in oceanography, has not yet been clarified.
    In this study, the authors investigated experimentally the fundamental behaviour of a two-dimensional water jet affected by sound, to find out the exact jet-sound relationships. The jet profile variables including the centerline velocity, the jet width, and the velocity distribution of the jet were measured with a hot film anemometer. Especially, the tendency of the velocity distribution of the jet was compared with Görtler's model.
    The following facts were confirmed:
    1) A water jet becomes sound-sensitive when both its Reynolds number and the frequency of sound are within some bounds.
    2) When a sound of certain frequency is applied, the jet centerline velocity increases but the velocity in the outer shear layer decreases. In this case, a sound-sensitive jet has a responsive frequency bandwidth involving the maximum value of centerline velocities which shifts towards a higher frequency with an increase in the Reynolds number.
    3) The tendency of the spread parameter shows that such changes in the velocity profile with the application of sound are related to the abrupt spreading of the jet following the transition from a laminar domain to a turbulent domain.
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