• Title/Summary/Keyword: heating space

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Preparation and Characterization of Polyimide/Carbon Nanotube Composites by in-situ Polymerization (In-situ 중합법에 의한 Polyimide/Carbon Nanotube 복합재료의 제조 및 특성)

  • Seo, Min-Kang;Park, Soo-Jin
    • Proceedings of the Korean Fiber Society Conference
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    • 2003.10b
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    • pp.223-224
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    • 2003
  • Polyimides (PI) are widely used in applications ranging from microelectronics to aerospace. Due to their insulating nature, significant accumulation of electrostatic charge may result on their surface, causing local heating and premature degradation to electronic components or space structures. Over the past decade, several publications have been made in fabrication and charaterization of CNT nanocomposites [1,2]. (omitted)

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Experimental Study on the Honeycomb Structure Collector (벌집형구조 집열기의 실험연구)

  • Lee, Jong-Ho
    • Solar Energy
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    • v.7 no.2
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    • pp.54-64
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    • 1987
  • Experiments on honeycomb structure collectors (HSC with/without cover) were performed and the experimental results showed good agreement with the preceding analytical results. The tendency of the efficiency of HSC was same with that of conventional air-type solar collector, even though there were some seasonal differences. Therefore, HSC, which can be itself utilized as a part of building structure, is applicable to space heating as well as preheating of industrial process and drying.

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A Study on Surface Temperature Patterns in the Tokyo Metropolitan Area Using ASTER Data

  • Fukui, Yuko
    • Proceedings of the KSRS Conference
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    • 2003.11a
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    • pp.1457-1459
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    • 2003
  • This study reports the surface temperature pattern of the Tokyo Metropolitan area using the ASTER surface temperature product. The product is an image processed by applying temperature-emissivity separation to atmospheric corrected infrared thermal radiance of the land surface, then converted to surface temperature by using Planck's function. Daytime and nighttime observation in a cold season and a warm season were used in this study. As a result, 1) contrast between urban and suburban, 2) extraction of heating area in urban, 3) measurement of cooling effect of green space were achieved.

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Discovery of highly dynamic and recurrent jets in a polar coronal hole observed by Hinode/SOT

  • Cho, Il-Hyun;Moon, Yong-Jae;Cho, Kyung-Suk
    • The Bulletin of The Korean Astronomical Society
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    • v.44 no.1
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    • pp.50.4-50.4
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    • 2019
  • We detect a new population of chromospheric jets in a polar coronal hole observed by Hinode/SOT. The propagating speed of the jets ranges in 30 - 490 km/s whose duration time is 3 - 52 s. The recurrent rate is approximately 3/min for a give segment of 1 arc-second horizontal interval. These jets are seemed to be more transient and faster than type II spicules at chromosphere, while the properties are compatible with the network jets seen in emission lines of transition region. We will discuss the implication of these jets for a coronal heating.

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Changes volatile flavor components of Korean Agrimonia Japonica by cooking (조리에 따른 한국산 짚신나물(Agrimonia Japonica)의 휘발성 풍미 성분의 변화)

  • 이혜정;이경희;구성자
    • Korean journal of food and cookery science
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    • v.11 no.2
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    • pp.122-125
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    • 1995
  • An attempt was made to determine the effect of the volatile components of edible wild grass by cooking. We collect the volatile components of Agrimonia Japonica by dynamic\ulcorner head space method. Samples were analyzed by gas chromatography-mass spectrometry(GC-MS). Thirty-six components, including 16 hydrocarbons, 7 alcohols, 4 esters, 7 benzoid compounds, 1 aldehyde and 1 ketone were confirmed in raw samples. Also 6 hydrocarbons identified in cooked sample. Alpha-pinene and 3-he-xane-ol were regarded as the most abundant components in raw sample. By heating of Japonica, most of the volatile compounds were disappeared, but alpha-pinene was remained abundantly.

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Reference Trajectory Analysis of Atmosphere Re-entry for Space Vehicle (우주비행체의 대기권 재진입 기준궤적 해석)

  • 이대우;조겸래
    • Journal of the Korean Society for Precision Engineering
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    • v.17 no.6
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    • pp.111-118
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    • 2000
  • The design of reference trajectory with respect to drag acceleration is necessary to decelerate from hypersonic speed safely after atmosphere re-entry of space vehicle. The re-entry guidance design involves trajectory optimization, generation of a reference drag acceleration profile with the satisfaction of 6 trajectory constraints during the re-entry flight. This reference drag acceleration profile can be considered as the reference trajectory. The cost function is composed of the accumulated total heating on vehicle due to the reduction of weight. And a regularization is needed to prevent optimal drag profile from varying too fast and achieve realized trajectory. This paper shows the relations between velocity, drag acceleration and altitude in drag acceleration profile, and how to determine the reference trajectory.

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Numerical Analysis on 3-dimensional Heat transfer of Heating Surface with Periodically Arrayed Injectors (분사기가 주기적으로 배열된 가열면의 3차원 열전달 수치해석 연구)

  • Cho, Won-Kook;Kim, Young-Mog
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.8
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    • pp.112-119
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    • 2002
  • Three dimensional numerical heat transfer analysis was carried out against periodically arranged fuel injectors of the liquid rocket engine. A finite volume method based on SIMPLE algorithm was adapted which gave a good agreement with the published results of the heat transfer problem of a backward facing step. The Nusselt number and pressure drop increased as the distance between the injector elements decreased. When the Reynolds number increased, the Nusselt number increased but nondimensionalized pressure drop decreased slightly.

UBV PHOTOMETRY AT THE OUTSIDE ECLIPSE PHASE OF AZ CASSIOPEIAE

  • Nha, Il-Seong
    • Journal of Astronomy and Space Sciences
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    • v.11 no.1
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    • pp.21-30
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    • 1994
  • VV Cep-type long period spectroscopic-eclipsing binary AZ Cas has been observed for five years, 1985 Oct~1990 Feb, UBV at the Ilsan Station of Yonsei University Observatory. A total of 431 observations (U=129, B=142 and V=160) are made for 86 nights. Instrumental differential UBV and B-V light curves made with these observations cover phases nearly a half of one period. There is no appreciable light variation in V but in other two passbands a gradual decrease of the brightness is clearly noticed. The loss of light in B resulted in a reddening in $\Delta(B-V)$ by + 0.06 at phases between 0.4~0.5 as compared with that of at phase ~0.1. This intrinsic reddening arouses a question why at the orbital phase of the transit of a hot star in front of a cool M supergiant the heating of the facing hemisphere of M supergiant by the strong radiation from the B stat is absent. With regard to this unusual situation we propose a hypothesis that a large amount of gas stream of low temperature ejected from the surface of M supergiant component towards the B star dominates the brightness of B star and the reflection effect.

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Modification of a cosmological hydrodynamic code for more realistic baryonic physics

  • Chun, Kyungwon;Shin, Jihye;Kim, Sungsoo S.
    • The Bulletin of The Korean Astronomical Society
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    • v.39 no.2
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    • pp.45.1-45.1
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    • 2014
  • structure of matters of Lambda cold dark matter (CDM) cosmology on detailed numerical simulations. To accomplish our research goal, we have added the following baryonic physics on the existing cosmological hydrodynamic code, Gadget-2: 1) radiative heating and cooling, 2) reionization of the Universe and UV shielding, 3) star formation, 4) energy and metallicity feedback by supernova. In addition, we included cluster formation to distinguish clustered star formation inside the very high density gas clumps from the field star formation. Our simulations cover a cubic box of a side length 4Mpc/h with 130 million particles. The mass of each particles is $3.4{\times}104Msun$, thus the GCs can be resolved with more than hundreds particles. We discuss various properties of the GCs such as mass function, specific frequency, baryon-to-dark matter ratio, metallicity, spatial distribution, and orbit eccentricity distribution as functions of redshift. We also discuss how the formation and evolution of the GCs are affected by UV shielding.

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Numerical simulation of turbulent air-flow in a closed engine room with heat source in a ship (열원이 있는 밀폐된 선박 기관실에서의 난류기류에 관한 수치적 연구)

  • 박찬수
    • Journal of Advanced Marine Engineering and Technology
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    • v.22 no.1
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    • pp.100-107
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    • 1998
  • Ventilation of the marine engine room is very important for the health of the workers as well as the nomal operation of machines. To find proper ventilation conditions of this engine room, numerical simulation with standard k-.epsilon. model was carried out. In the present study, the marine engine room is considered as a closed space with a heat source and forced ventilation ducts. The injection angle of air supply is found to be important. Injection with downword angle depresses recirculation flow, causing a strong steam in the wider space of the room. Ventilation and removal of the released heat are promoted with this pattern. There is a possibility of local extreme heating at the upper surface of engine when supply and exhaust ports of air are in bilateral symmetry. The effect of the increase of exhaust port area on ventilation decreases as the number of supply port increases.

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