• 제목/요약/키워드: liftoff temperature

검색결과 17건 처리시간 0.024초

고온 동축류버너에서 층류부상화염 특성 (Characteristics of Laminar Lifted Flame In High Temperature Coflow Burner)

  • 김길남;원상희;차민석;정석호
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2001년도 제23회 KOSCO SYMPOSIUM 논문집
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    • pp.104-110
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    • 2001
  • Characteristics of lifted flame for highly diluted propane with nitrogen in high temperature coflowing air have been experimentally investigated, and the stabilization mechanism of lifted flame in high temperature air coflow have been proposed. As the coflow temperature increases, the liftoff height of flame decreased due to the increase of stoichiometry laminar burning velocity. At same coflow temperature, the difference of liftoff height between the fuel mole fractions has been disappeared by scaling the liftoff velocity with stoichiometry laminar burning velocity. It has been found that lifted flame can be stabilized for even smaller fuel velocity than stoichiometry laminar burning velocity. This can be attributed to buoyancy effect and the liftoff velocity characteristics for coflow temperature support it.

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동축류 제트에서 초기 온도 변화에 따른 난류 부상화염 특성 (Characteristics of Turbulent Lifted Flames in Coflow Jet with Initial Temperature Variations)

  • 김길남;원상희;정석호
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2004년도 제28회 KOSCO SYMPOSIUM 논문집
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    • pp.15-20
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    • 2004
  • Characteristics of turbulent lifted flames in coflow jet have been investigated by varying initial temperature through the heating of coflow air. In the turbulent regime, liftoff height increases linearly with fuel jet velocity and decreases nonlinearly as the coflow temperature increases. This can be attributed to the increase of turbulent propagation speed, which is strongly related to laminar burning velocity. Dimensionless liftoff heights are correlated well with dimensionless jet velocity, which are scaled with parameters determining local flow velocity and turbulent propagation speed. This implies that the turbulent lifted flames are stabilized by balance mechanism between local turbulent burning velocity and flow velocity. Blowout velocity can be obtained from the ratio of mixing time to chemical time. Comparing to previous researches, thermal diffusivity should be evaluated from the initial temperature instead of adiabatic flame temperature.

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동축류 제트에서 초기 온도 변화에 따른 난류 부상화염 특성 (Characteristics of Turbulent Lifted Flames in Coflow Jet with Initial Temperature Variations)

  • 김길남;원상희;정석호
    • 한국연소학회지
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    • 제9권1호
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    • pp.32-38
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    • 2004
  • Characteristics of turbulent lifted flames in coflow jet have been investigated by varying initial temperature through the heating coflow air. In the turbulent regime, liftoff height increases linearly with fuel jet velocity and decreases nonlinearly as the coflow temperature increases. This can be attributed to the increase of turbulent propagation speed, which is strongly related to laminar burning velocity. Dimensionless liftoff heights are correlated well with dimensionless jet velocity, which are scaled with parameters determining local flow velocity and turbulent propagation speed. This implies that the turbulent lifted flames are stabilized by balance mechanism between local turbulent burning velocity and flow velocity. Blowout velocity can be obtained from the ratio of mixing time to chemical time. Comparing to previous researches, thermal diffusivity should be evaluated from the initial temperature instead of adiabatic flame temperature.

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PRELAUNCH THERMAL ANALYSIS OF KSLV-I PAYLOAD FAIRING

  • Choi Sang-Ho;Kim Seong-Lyong;Kim Insun
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2004년도 한국우주과학회보 제13권2호
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    • pp.356-359
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    • 2004
  • Prelaunch thermal analysis of the KSLV (Korea Space Launch Vehicle)-I PLF (Payload Fairing) was performed to predict maximum/minimum liftoff temperatures and to evaluate of air conditioning performance. Prelaunch thermal analysis includes internal air conditioning effect, external convective heating/cooling, radiation exchange with the ground and sky, radiation between spacecraft and PLF, and solar radiation incident on PLF. Analysis was performed at two extreme conditions, hot day condition and cold day condition. The results showed that the maximum liftoff temperature was $53^{\circ}C$ and the minimum liftoff temperature was $-3.8^{\circ}C$. It was also found that conditioned air supplying, in $20{\pm}2^{\circ}C\;and\;1200\;m^3/hr$, is sufficient to keep the internal air in required temperature range.

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자발화된 메탄 부상화염에 대한 수소 첨가의 영향 (Effect of Hydrogen Addition on Autoignited Methane Lifted Flames)

  • 최병철;정석호
    • 대한기계학회논문집B
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    • 제36권1호
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    • pp.75-81
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    • 2012
  • 고온의 동축류 공기와 수소가 함유된 메탄 연료제트에서 자발화된 층류 부상화염의 특성을 실험적으로 조사하였다. 그 결과로 순수 메탄 제트에서 자발화되는 경계 온도인 920 K 를 초과하는 초기 온도에서 메탄/수소 혼합기의 자발화된 부상화염은 연료 몰분율에 따라 삼지화염 또는 마일드 연소를 보였고, 제트속도에 따라 부상화염의 높이가 증가하는 전형적인 특성을 보였다. 소량의 수소가 첨가된 부상화염의 높이는 메탄의 경우와 유사하게 단열적 점화지연시간의 2 승에 대한 의존성이 유지되었다. 반면에, 초기 온도가 920 K 미만인 경우에서 화염은 수소의 점화 촉진에 의해서 자발화 되었다. 그리고 제트속도가 증가함에 따라 자발화된 부상화염의 높이는 비선형적으로 감소하는 독특한 특성을 보였으며, 수소의 선호확산이 그 현상에 대해서 중요한 역할을 할 것으로 예상된다.

고온 동축류에서 층류 화염의 부상특성 (Characteristics of Laminar Lifted Flame in High Temperature Coflow)

  • 김길남;원상희;차민석;정석호
    • 한국연소학회지
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    • 제7권2호
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    • pp.1-6
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    • 2002
  • Characteristics of laminar lifted flames of propane highly-diluted with nitrogen have been investigated at various temperatures of coflow air. At various fuel mole fractions, the base of laminar lifted flames has the structure of tribrachial (or triple) flame. The liftoff heights are correlated well with the stoichiometric laminar burning velocity considering initial temperature at a given coflow velocity. It shows that lifted flames are stabilized on the basis of the balance mechanism between local flow velocity and the propagation speed of tribrachial flame, regardless of the temperature of coflow and fuel mole fraction. Lifted flames exist for a jet velocity even smaller than the stoichiometric laminar burning velocity, and liftoff velocity increases more rapidly than stoichiometric laminar burning velocity as coflow temperature increases. These can be attributed to the buoyancy effect due to the density difference.

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초기 온도 변화를 갖는 동축류 제트에서 메탄 난류 부상화염의 특성 (Characteristics of Methane Turbulent Lifted Flames in Coflow Jets with Initial Temperature Variation)

  • 최병철;정석호
    • 대한기계학회논문집B
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    • 제32권12호
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    • pp.970-976
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    • 2008
  • Characteristics of methane turbulent non-premixed flame have been studied experimentally in coflow jets with initial temperature variation. The results showed that the premixed flame model and the large-scale mixing model for turbulent flame stabilization were effective for methane fuel considered initial temperature variation. Especially, the premixed flame model has been improved by considering nitrogen dilution for the liftoff height of turbulent lifted flame. In estimating blowout velocity and the liftoff height at blowout with the premixed flame model and the large-scale mixing model, the two turbulent models were excellently correlated by considering the effect of physical properties and buoyancy for the initial temperature variation.

이산화탄소 재순환이 순산소 난류제트 확산화염에 미치는 영향 (Effects of $CO_{2}$ Recirculation on Turbulent Jet Diffusion Flames with Pure Oxygen)

  • 차민석;김호근;김한석;안국영
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 제26회 KOSCO SYMPOSIUM 논문집
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    • pp.255-260
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    • 2003
  • Characteristics of methane jet diffusion flames using pure oxygen with recirculating $CO_{2}$ as an oxidizer were investigated experimentally. A coflow burner was considered, and the diameter of confinement was larger than that of the coflow. No stabilized flame could be observed over 75% of $CO_{2}$ volume percent. A comparison between air and $O_{2}/CO_{2}$ mixture was made in terms of liftoff velocity, flame liftoff height, and blowout conditions. As results, more stable flame could be observed with $O_{2}/CO_{2}$ mixture for the case of having similar flame temperature.

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발사전 가열 해석 - Delta II 자료 분석

  • 최상호;김성룡;김인선
    • 항공우주기술
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    • 제4권2호
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    • pp.126-134
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    • 2005
  • 발사체는 발사되기 수일 전에 발사탑에 세워져 체크과정 및 연료공급 등을 수행하게 되므로 발사까지는 계속 외부의 열환경에 노출되게 된다. 발사체의 페어링에 대한 발사전 가열 해석(Prelaunch Thermal analysis)은 발사시 페어링의 최대/최소 온도 예측 및 공조 설비(air conditioning system)의 성능 예측을 목적으로 수행된다. 본 연구에서는 범용 열해석 프로그램인 Sinda/Fluint 이용하여 Delta II 페어링에 대하여 발사전 가열 해석을 수행하였으며, 그 결과를 Delta II 보고서 자료와 비교 및 분석하였다.

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