• Title/Summary/Keyword: 케로신-공기 혼합물

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Numerical Investigation of Dynamic Responses of a Thermal Elasto-plastic Tube under Kerosene-air Mixture Detonation (케로신-공기 혼합물의 데토네이션 하중에 의한 열탄소성 관의 동적 거동 해석)

  • Gwak, Min-cheol;Lee, Younghun;Yoh, Jai-ick
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.5
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    • pp.60-69
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    • 2016
  • This paper presents a numerical investigation on kerosene-air mixture detonation and behaviors of thermal elasto-plstic thin metal tube under detonation loading based on multi-material analysis. The detonation loading is modeled by the kerosene-air mixture detonation which is compared with Chapman-Jouguet (C-J) condition and experimental cell size. To conform the elasto-plastic model, plastic and elastic behaviors are verified by Taylor impact and plate bending motion, respectively. The numerical results are compared with the theory on burst pressure of tube. The critical deformable thickness with the thermal softening considered is good agreement with the theoretical value.

Numerical Analysis of Responses of a Elasto-plastic Tube under Kerosene-air Mixture Detonation (케로신-공기 혼합물의 비정상연소 모델과 탄소성 관의 동적 거동 수치해석)

  • Lee, Younghun;Gwak, Min-cheol;Yoh, Jai-ick
    • 한국연소학회:학술대회논문집
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    • 2015.12a
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    • pp.169-172
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    • 2015
  • This paper presents a numerical investigation on kerosene-air mixture detonation and behaviors of thermal elasto-plstic thin metal tube under detonation loading based on multi-material analysis. The detonation loading is modeled by the kerosene-air mixture detonation which is compared with CJ condition and experimental cell size. And the thermal softening effect on elasto-plstic model of metal tube is indicated by different dynamic response of detonation loaded tube in various temperature and tube thickness.

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Numerical Analysis of Detonation of Kerosene-Air Mixture and Solid Structure (케로신-공기 혼합물의 데토네이션 모델과 구조체 모델을 통한 금속관의 수치해석)

  • Lee, Younghun;Gwak, Min-Cheol;Yoh, Jai-Ick
    • Journal of the Korean Society of Propulsion Engineers
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    • v.19 no.2
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    • pp.29-37
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    • 2015
  • This paper presents a numerical investigation on detonation of a kerosene-air mixture in the copper tube and the structural response associated with combustion instability in liquid rocket engine. A single step Arrehnius rate law and Johnson-Cook strength model are used to describe the chemical reaction of kerosene-air mixture detonation and the plastic deformation of the copper tube. The changes of flow field and tube stress which are induced by plastic deformation, are investigated on the different tube thicknesses and nozzle configurations.