• Title/Summary/Keyword: 비열비

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Self-Sustained Tone Simulations using the Finite Difference Lattice Boltzmann Method with Flexible Specific Heat Ratio (조정 가능한 비열비를 갖는 FDLBM에 의한 자려발생 음의 시뮬레이션)

  • Oh, S.K.;Ahn, S.W.;Kim, J.W.;Kang, H.K.
    • Journal of Power System Engineering
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    • v.11 no.1
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    • pp.82-91
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    • 2007
  • 기존의 2차원 FDLB 모델(D2Q21)에서 비열비 ${\gamma}$는 공간의 차원수(D)에 의존한다. 즉, 2차원 공간의 계산에서는 ${\gamma}=(D+2)/D=2.0$밖에 취할 수 없으며, 공기와 같은 실체기체를 전산모사 하기에는 여러 어려움이 있다. 이러한 이유 때문에 문헌[1]의 LBM에서 제안된 조정 가능한 비열비 모델을 2차원 FDLB모델에 적용하여 자려발생 에지톤(edgetone)의 수치계산이 수행되었다. wedge의 선단각도가 ${\alpha}=23^{\circ}$(Case I) 및 $20^{\circ}$(Case II)를 갖는 2가지 모델이 설정되었으며, 노즐출구에서 wedge선단까지의 거리 w/d는 $3d{\sim}12d$사이에서 주어졌다. edgetone은 노즐로부터 나온 분류와 edge의 상호작용으로 이난 음압(sound pressure)의 차에 의해서 소음이 발생하며, 이 음압은 다시 상류의 분류에 영향을 미쳐 분류의 변동을 가져온다. w/d가 ??9d이하인 경우, 피드백(feedback) 메커니즘에 기인한 주기적인 운동이 발생하지만, w/d가 큰 ??9d이상인 경우에는 분류의 불안정성 때문에 규칙적인 분류의 운동은 보이질 않으며, 이는 기존의 연구결과들과 잘 일치함을 보였다. 본 연구에서 적용된 모델을 이용하여 공기와 같은 2원자 기체의 비열비 ??${\gamma}=1.4$를 갖는 유체에 있어서 공력 소음의 수치예측이 가능하다는 것을 확인하였다.

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Characteristic Study of Micro-Nozzle according to the Ratio of Nozzle Expansion and Specific heats (노즐 팽창비와 비열비에 따른 마이크로 노즐의 특성연구)

  • Oh Hwayoung;Huh Hwanil;Moon Seonghwan
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.381-385
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    • 2005
  • Recently, spacecraft technology trends can be expressed three words, i.e. 'faster, cheaper and smaller'. Among these systems, micro propulsion device is an essential component. Also micro nozzle is the most important part in the micro propulsion device. In case of cold-gas thruster, micro nozzle converts the stored energy in a pressurized gas into kinetic energy through expansion ratio. In this paper we report characteristics of micro nozzle with throat expansion ratio and ratio of specific heats. We measure thrusts using strain gauge based thrust measurement system. We can estimate the micro nozzle performance through experiments.

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Combustion Characteristics of High Pressure Gas Generator for Liquid Rocket Engine (액체로켓엔진용 가스발생기의 고압연소특성)

  • Han Yeoung-Min;Lee Kwang-Jin;Moon Il-Yoon;Seo Seong-Hyeon;Choi Hwan-Seok;Lee Soo-Yong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.341-345
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    • 2005
  • This paper is for the combustion characteristics of gas generator which drive 1.5MW-class turbo pump and runs in fuel-rich combustion regime with LOx/kerosene as propellant. The outline of development procedure of real scale high pressure gas generator is introduced and the relation between O/F ratio and outlet temperature and the molecular weight and specific heat ratio of combustion gas are described. The relation between O/F ratio and temperature is newly obtained at higher pressure and the molecular weight and specific heat ratio is modified and their validity is confirmed by the mass relation equation.

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A Study on Physicochemical Characteristics of Hydrogen Gas Explosion (수소가스 폭발의 물리화학적 특성 연구)

  • Jo, Young-Do
    • Journal of the Korean Institute of Gas
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    • v.16 no.1
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    • pp.8-14
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    • 2012
  • Hydrogen is considered to be the most important future energy carrier in many applications reducing significantly greenhouse gas emissions, but the explosion safety issues associated with hydrogen applications need to be investigated and fully understood to be applicable as the carrier. The risk associated with a explosion depends on an understanding of the impacts of the explosion, particularly the pressure-time history during the explosion. This work provides the effects of explosion parameters, such as specific heat ratio of burned and unburned gas, equilibrium maximum explosion pressure, and burning velocity, on the pressure-time history with flame growth model. The pressure-time history is dominantly depending on the burning velocity and equilibrium maximum explosion pressure of hydrogen-air mixture. The pressure rise rate increase with the burning velocity and equilibrium maximum explosion pressure. The specific heat ratio of unburned gas has more effect on the final explosion pressure increase rate than initial explosion pressure increase rate. However, the specific heat ratio of burned gas has more influence on initial explosion pressure increase rate. The flame speeds are obtained by fitting the experimental data sets. The flame speeds for hydrogen in air based on our experimental data is very low, making a transition from deflagration to detonation in a confined space unlikely under these conditions.

비열평형 대기의 원자스펙트럼

  • Kim, Gap-Seong
    • Publications of The Korean Astronomical Society
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    • v.5 no.1
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    • pp.40-64
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    • 1990
  • 복사전달식, 통계평형식 및 전하 입자 보존식을 동시에 만족시키는 비열평형상태의 대기에 대하여 그 방출원자스펙트럼을 수치계산하였다. 등온, 중압의 비열평형 태양홍염을 대상모델로 선정하였는데 여기에 적응한 제한조건중 복사전달에 관련된 편미분방정식은 3점 근사 차분법에 의해 정리하였고 홍염중심에 대칭성을 가정하여 경제조건을 부여하였으며 대기의 물리상태에 관련된 비선형 연립방정식의 해는 완전선형화 기법을 통한 퓨트리에 소거법을 이용해 구하였다.

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디퓨져의 확대각이 임계노즐 유동에 미치는 영향

  • 김재형;김희동
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2002.04a
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    • pp.31-32
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    • 2002
  • 임계노즐(critical nozzle)은 유동을 유로 최소단면부에서 초크시켜, 질량유량을 계측하기 위한 일종의 유체기구로, 최근 다양한 분야에서 널리 활용되고 있다. 압축성 기체역학의 관계식에 의하면, 임계노즐을 통하는 기체유동의 이론적인 질량유량은 노즐 목의 직경, 노즐 상류의 온도와 압력 그리고 기체의 비열비 등의 함수로 주어진다 그러나 실제 유동에서는 점성과 열전달 등의 초과로 인하여, 이론적 질량 유량과 실제유량의 비 즉 유출계수(discharge coefficient)의 값은 1.0으로 되지 않는다.

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Characteristic Study of Micro-Nozzles according to the Ratios of Nozzle Expansion and Specific heats in low vacuum condition (저진공상태에서 노즐 팽창비와 비열비에 따른 마이크로 노즐의 특성 연구)

  • Kim, Youn-Ho;Jung, Sung-Chul;Huh, Hwan-Il
    • 유체기계공업학회:학술대회논문집
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    • 2006.08a
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    • pp.249-252
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    • 2006
  • We conducted the experiment to analyze characteristics of micro-nozzle using different cold gas under two different nozzle expansion ratios in low vacuum condition. We measured thrust and chamber pressure and mass flow rate under low vacuum condition, and then compared them with those in ambient pressure.

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The effects of primary gas physical properties on the performance of annular injection type supersonic ejector (주유동 기체의 물리적 특성이 환형 분사 초음속 이젝터의 성능에 미치는 영향)

  • Jin, Jung-Kun;Kim, Se-Hoon;Park, Geun-Hong;Kwon, Se-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.12
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    • pp.68-75
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    • 2005
  • The effects of the physical properties of primary flow on the performance of a supersonic ejector were investigated. Axisymmetric annular injection type supersonic ejector was used for the study of the effects of molecular weight and the specific heat at constant pressure on the ejection performance. Test gases include; air, $CO_{2}$, Ar, $C_{3}H_{8}$, and $CCl_{2}F_{2}$ for different values of gas properties. As the molecular weight and CP of the primary gas increase, the secondary flow pressure increases at the same primary stagnation pressure and this behavior results from the combined effects of molar specific heat or specific heat ratio.

Design of a 10× Zoom Lens with an Expander for an MWIR Camera Using Athermal Material Composition Method (비열화 소재 구성 방법을 이용한 중적외선 카메라용 확장형 10배 줌 렌즈 설계)

  • Ryu, Tae-Sik;Park, Sung-Chan
    • Korean Journal of Optics and Photonics
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    • v.33 no.6
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    • pp.287-294
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    • 2022
  • This study presents a method for designing an athermal middle wavelength infrared (MWIR) zoom lens with the iterative selection of material compositions on an athermal glass map. The optical properties of glass for MWIR are generally very sensitive to temperature, compared with visible glass. To compensate for focus error due to temperature change, the non-athermalized zoom system requires a large amount of movement of a compensator, which results in an unstable zoom system. To solve this problem, the material compositions for an athermal zoom lens have effectively been obtained using the thermal aberration correction process analytically on an athermal glass map. An expander lens is used to enlarge the focal lengths of an original main zoom lens two times. Finally, while this expander is attached to an original athermal zoom system, the final zoom system equipped with this expander doubles the focal length ranges and has stable performance over a specified temperature range.

Properties of Alcohol Fermentation from Barley Treated with Non-steam and Steam (비열 및 열처리에 따른 보리의 알코올발효 특성)

  • Woo, Seung-Mi;Kim, Tae-Young;Yeo, Soo-Hwan;Kim, Sang-Bum;Jeong, Yong-Jin
    • Food Science and Preservation
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    • v.14 no.2
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    • pp.201-206
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    • 2007
  • This study was designed to investigate quality characteristics of alcohol fermentation from 5 barldy cultivars teated with non-steam and steam. In alcohol fermentation treated with non-steam, alcohol concentration reached to 1.7% for naked berley, 2.9% for naked waxy barley and 4.3% for Hinchalssalbori. However, no fermentation was occurred with baney and waxy barley. When the barley cultivars were steamed, alcohol concentrations showed to be higher than those not steamed. In sugar concentration from non-steam, both barley and waxy barley showed to have approximately $9.0\;^{\circ}Brix$ and naked barley, naked waxy barley and Hinchalssalbori showed to have approximately $5.0\;^{\circ}Brix$. When the burley cultivars were steamed, sugar concentration was decreased as alcohol concentration was increased Interestingly, sugar concentrations in barley cultivars were fast dropped more than 50% following alcohol fermentation except naked barley k alcohol fermentation treated with non-steam, total acidity of Hinchalssalbori was 0.51%, but the others showed more than 0.80%. So except for Hinchalssalbori, it was possible that acidification occurred during the fermentation. In total acidity from steam, all samples showed less than 0.3%. In flee sugar from non-steam, total free sugar contents of barley and waxy barley were approximately 4,000.0mg% and contents of naked barley naked waxy barley and Hinchalssalbori were each approximately 300.0 mg%. Free sugar from steam was increased as sugar concentration increased. In conclusion, barley cultivars were evaluated to be not suitable at alcohol fermentation treated with non-steam.