• 제목/요약/키워드: radiative cooling

검색결과 123건 처리시간 0.02초

CMC 모델을 이용한 난류 비예혼합 Syngas 화염장 해석 (Fully coulpled CMC modeling for three-dimensional turbulent nonpremixed syngas flame)

  • 김군홍;이정원;김용모;안국영
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2006년도 제32회 KOSCO SYMPOSIUM 논문집
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    • pp.111-120
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    • 2006
  • The fully coupled conditional moment closure(CMC) model has been developed to realistically simulate the structure of complex turbulent nonpremixed syngas flame, in which the flame structure could be considerablyl influenced by the turbulence, transport history, and heat transfer as well. In order to correctly account for the transport effect, the CMC transport equations fully coupled with the flow and mixing fields are numerically solved. The present CMC approach has successfully demonstrated the capability to realistically predict the detailed structure and the overall combustion characteristics. The numerical results obtained in this study clearly reveal the importance of the convective and radiative heat transfer in the precise structure and NOx emission of the present confined combustor with a cooling wall.

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전자부품의 인쇄회로기판 부착시 적외선 Reflow Soldering과정 열전달 해석 (Heat Transfer Analysis of Infrared Reflow Soldering Process for Attaching Electronic Components to Printed Circuit Boards)

  • 손영석
    • Journal of Welding and Joining
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    • 제15권6호
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    • pp.105-115
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    • 1997
  • A numerical study is performed to predict the thermal response of a detailed card assembly during infrared reflow soldering. The card assembly is exposed to discontinuous infrared panel heater temperature distributions and high radiative/convective heating and cooling rates at the inlet and exit of the oven. The convective, radiative and conduction heat transfer within the reflow oven as well as within the card assembly are simulated and the predictions illustrate the detailed thermal responses. The predictions show that mixed convection plays an important role with relatively high frequency effects attributed to buoyancy forces, however the thermal response of the card assembly is dominated by radiation. The predictions of the detailed card assembly thermal response can be used to select the oven operating conditions to ensure proper solder melting and minimization of thermally induced card assembly tresses and warpage.

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Migration of Radiative Gas Giants with GIZMO

  • Yang, Seung-Won;Kim, Woong-Tae
    • 천문학회보
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    • 제44권1호
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    • pp.47.1-47.1
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    • 2019
  • A gas giant formed in a massive protoplanetary disk via gravitational instability migrates inward due to its gravitational interaction with the disk. Planet migration occurs in various ways depending on the disk structure and internal processes, but previous studies only considered quantitative radiative feedback resulting from mass accretion onto the planet. Allowing for accretion feedback, we perform three-dimensional hydrodynamic simulations with GIZMO to investigate orbital evolution of giant planets in a protoplanetary subject to -cooling. This work shows a planet gains mass due to accretion and gradually opens a gap as it moves inward. The migration in the end halts when the planet clears the gas around its orbit. A more massive planet grows its mass faster and migrates more rapidly, stalling at an orbit farther away from the protostar. Models with a cold disk readily construct a circumplanetary disk and result in high mass growth of the planet. Accretion feedback, in general, reduces the rate of the planet growth and delays migration. We discuss our results with GIZMO in comparison with the previous results with different codes.

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막냉각 효과를 고려한 액체로켓 엔진의 연소 특성에 관한 연구 (A Numerical Study on the Combustion Characteristics in a Liquid Rocket Engine with Film Cooling Effect)

  • 변도영;김만영;백승욱
    • 한국항공우주학회지
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    • 제31권8호
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    • pp.69-76
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    • 2003
  • 액체로켓 연소기 내의 막냉각 특성 분석을 위한 비회체 분무연소에 대한 수치해석을 수행하였다. 막냉각 연료의 특성에 따른 연소기 벽면의 온도변화를 살펴보기 위하여 막냉각용 연료의 유랑, 막냉각용 액적의 직경, 그리고 공기/연료 혼합비를 매개변수로 한 수치해석을 수행하여 연소기 벽면의 온도는 막냉각용 연료 액적 직경의 변화에는 큰 영향을 받지 않지만 막냉각용 연료 유량 및 공기/연료 혼합비에 영향을 받고 있음을 확인하였다. 또한, 추진기관 벽면으로 전달되는 전도 및 복사열유속을 고찰함으로서 이러한 액체 추진기관의 연소특성을 이해하기 위해서는 열복사 및 물성치의 적절한 고찰이 필요함을 지적하였다.

액체로켓엔진 노즐확장부 소재기술 동향 (Material Trends of Nozzle Extension for Liquid Rocket Engine)

  • 이금오;유철성;최환석
    • 항공우주산업기술동향
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    • 제9권1호
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    • pp.139-149
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    • 2011
  • 액체 로켓 엔진의 연소기는 높은 온도의 연소가스를 발생시키므로 연소실과 노즐은 열적으로 보호되어야 한다. 고공 엔진의 노즐확장부도 고열에 견딜 수 있게 설계되어야 하며, 이를 위하여 가스냉각, 삭마냉각, 복사냉각등 다양한 방법의 냉각이 적용되고 있다. 특히 큰 노즐 팽창비를 갖는 상단엔진의 경우 무게가 발사체 성능에 미치는 영향이 크므로 경량 내열 소재가 개발되어 사용되어 왔다. 미국과 러시아, 유럽에서 사용되어 온 노즐확장부 재료를 조사한 결과 스테인리스강과 티타늄합금과 같은 무거운 금속 재료에서 경량의 탄소섬유 강화 복합재 또는 세라믹 복합재로 바뀌어 가는 경향이 파악되었다.

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노즐 후방부의 Radiative Heat Flux 측정 (Measurement of Radiative Heat Flux of Nozzle Exit)

  • 안원근;박희호;황수권;김유
    • 한국항공우주학회지
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    • 제31권5호
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    • pp.87-92
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    • 2003
  • 일반적으로 연소과정에서 발생한 고온고압의 연소가스로 인하여 액체추진기관의 연소실 및 노즐 벽면 그리고 추진기관 후방부위에 대류열전달과 복사열전달이 발생하는 것으로 알려져 있으며, 액체추진기관에서 발생하는 복사열전달 현상은 재생냉각장치의 열입력랑 예측 및 발사체의 추진기관 후방부위에 탑재되는 전자장비 및 구조물의 열적 환경을 분석하는데 매우 중요하다. 이에 본 연구에서는 노즐 후방부위에서 발생하는 복사열전달량을 측정하고 연소압과 혼합비에 따른 영향을 파악하였다. 동알한 형상의 소형 액체추진기관에서 연소압(200, 300, 400 psi)과 혼합비(1.5, 2.0, 2.5)에 따른 복사열전달의 특성을 파악하기 위하여 각각 3가지 조건에 대하여 연소시험을 수행하여 복사열전달량을 측정하였다. 시험 결과로부터 연소가스에서 발생하는 복사열전달의 상대적인 크기 및 미치는 인자들을 파악할 수 있었다. 본 연구를 통하여 석영을 활용하여 복사하는 복사열전달의 크기 및 현상을 파악할 수 있었다. 또한, 연소실 및 노즐에서 발생하는 복사열전달 현상을 파악할 수 있었다

TURBULENCE PRODUCED BY TSUNAMIS IN GALAXY CLUSTERS

  • FUJITA YUTAKA;MATSUMOTO TOMOAKI;WADA KEIICHI
    • 천문학회지
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    • 제37권5호
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    • pp.571-574
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    • 2004
  • Clusters of galaxies are filled with X-ray emitted hot gas with the temperature of T ${\~}$2-10 keV. Recent X-ray observations have been revealing unexpectedly that many cluster cores have complicated, peculiar X-ray structures, which imply dynamical motion of the hot gas. Moreover, X-ray spectra indicate that radiative cooling of the cool gas is suppressed by unknown heating mechanisms (the 'cooling flow problem'). Here we propose a novel mechanism reproducing both the inhomogeneous structures and dynamics of the hot gas in the cluster cores, based on state-of-the-art hydrodynamic simulations. We showed that acoustic-gravity waves, which are naturally expected during the process of hierarchical structure formation of the universe, surge in the X-ray hot gas, causing a serous impact on the core. This reminds us of tsunamis on the ocean surging into an distant island. We found that the waves create fully-developed, stable turbulence, which reproduces the complicated structures in the core. Moreover, if the wave amplitude is large enough, they can suppress the cooling of the core. The turbulence could be detected in near-future space X-ray missions such as ASTRO-E2.

Mapping and Analyzing the Park Cooling Intensity in Mitigation of Urban Heat Island Effect in Lahore, Pakistan

  • Hanif, Aysha;Nasar-u-Minallah, Muhammad;Zia, Sahar;Ashraf, Iqra
    • 대한원격탐사학회지
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    • 제38권1호
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    • pp.127-137
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    • 2022
  • Urban Heat Island (UHI) effect has been widely studied as a global concern of the 21st century. Heat generation from urban built-up structures and anthropogenic heat sources are the main factors to create UHIs. Unfortunately, both factors are expanding rapidly in Lahore and accelerating UHI effects. The effects of UHI are expanding with the expansion of impermeable surfaces towards urban green areas. Therefore, this study was arranged to analyze the role of urban cooling intensity in reducing urban heat island effects. For this purpose, 15 parks were selected to analyze their effects on the land surface temperature (LST) of Lahore. The study obtained two images of Landsat-8 based on seasons: the first of June-2018 for summer and the second of November-2018 for winter. The LST of the study area was calculated using the radiative transfer equation (RTE) method. The results show that the theme parks have the largest cooling effect while the linear parks have the lowest. The mean park LST and PCI of the samples are also positively correlated with the fractional vegetation cover (FVC) and normalized difference water index (NDWI). So, it is concluded that urban parks play a positive role in reducing and mitigating LST and UHI effects. Therefore, it is suggested that the increase of vegetation cover should be used to develop impervious surfaces and sustainable landscape planning.

FUTURE SPACE INFRARED TELESCOPE MISSION, SPICA

  • MATSUMOTO TOSHIO
    • 천문학회지
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    • 제38권2호
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    • pp.89-91
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    • 2005
  • SPICA (Space Infrared Telescope for Cosmology and Astrophysics) is an infrared astronomical satellite with a 3.5 m cooled telescope which is very powerful in mid- and far- infrared observations and makes complementary role to JWST and Herschel. SPICA will be launched at ambient temperature without any cryogen into the Sun-Earth L2 orbit and cooled down in space to 4.5 K with use of efficient radiative cooling and mechanical coolers. The present status of SPICA and the developments of the satellite system are reported.

THE INSTABILITIES OF ACCRETION DISKS WITH RADIAL ADVECTION

  • WU XUE-BING
    • 천문학회지
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    • 제29권spc1호
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    • pp.231-232
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    • 1996
  • The local instabilities of accretion disks were extensively studied, with the considerations of radial advection, thermal diffusion and different disk geometry, dominated pressure and optical depth. Two inertial-acoustic modes in a geometrically thin, radiative cooling dominated disk depart from each other if very little advection is included. A geometrically slim, advection-dominated disk is found to be always stable if it is optically thin. However, if it is optically thick, the thermal diffusion has no effect on the stable viscous mode but has a significant contribution to enhance the thermal instability.

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