• Title/Summary/Keyword: 유동혼합기 또는 난류발생기

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Dynamic Stability Analysis of the Nuclear Fuel Rod Affected by the Swirl Flow due to the Flow Mixer (유동혼합기에 의한 회전유동을 고려한 핵연료 봉의 동적 안정성해석)

  • Lee, Kang-Hee;Kim, Hyung-Kyu;Yoon, Kyung-Ho
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2008.04a
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    • pp.641-646
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    • 2008
  • Long and slender body with or without flexible supports under severe operating condition can be unstabilized even by the small cross flow. Turbulent flow mixer, which actually increases thermal-hydraulic performance of the nuclear fuel by boosting turbulence, disturbs the flow field around the fuel rod and affects dynamic behavior of the nuclear fuel rods. Few studies on this problem can be found in the literature because these effects depend on the specific natures of the support and the design of the system. This work shows how the dynamics of a multi-span fuel rod can be affected by the turbulent flow, which is discretely activated by a flow mixer. By solving a state-space form of the eigenvalue equation for a multi-span fuel rod system, the critical velocity at which a fuel rod becomes unstable was established. Based on the simulation results, we evaluated how stability of a multi-spanned nuclear fuel rod with mixing vanes can be affected by the coolant flow in an operating reactor core.

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Unsteady Ignition in the Pulse Combustor with Counter Jet Flows (대향분출류가 있는 맥동연소기의 비정상 점화현상)

  • 이창진
    • Journal of the Korean Society of Propulsion Engineers
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    • v.1 no.1
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    • pp.64-72
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    • 1997
  • An analytical study has been performed to investigate the unsteady ignition characteristics of pulse combustion. In many combustion applications, strain rate of the flow can significantly affect the combustion features; ignition, extinction, and reignition. In the pulse combustion, two jets (hot combustion gases and fresh mixtures) coming from the opposite side of the combustor will collide in the combustor forming a stagnation region where the chemical reaction is suppressed by the strain rate until this becomes below the critical value. In this research, the method of large activation energy asymptotic is adopted with one step irreversible kinetics to examine the ignition response to the periodic variation of the strain rate of flow. The results show the variation of the maximum value of strain rate can determine whether the ignition or extinction occur.

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