• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집B
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• pp.688-692
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• 2001

Three-dimensional experimental analyses were conducted in the pulverizer simplified isothermal model. The experimental model was constructed on a 1/3.5 scale of 500MW pulverized coal boiler. The purpose of this study is to investigate the characteristics of coal particle separator and the pressure loss in the pulverizer models with dynamic classifier. Without regards a shape of separator top, the results showed that the increase of dynamic classifier rpm was induced in finer coal particle. But the capacity of total mass per minute was reduced. Also, the increase of dynamic classifier rpm had no effect on total pressure loss, but an increase of inlet velocity was induced that the rise of total pressure loss in the pulverizer models with dynamic classifier.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2011년도 추계학술대회 초록집
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• pp.39.2-39.2
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• 2011

The new and renewable energy today has a great interest in all countries around the world. In special it has need more limit of the fossil fuel that needs of low carbon emission among the social necessary conditions. Recently, the high-rise building demand the structural safety, the economic feasibility and the functional design. The high-rise building spends enormous energy and it satisfied the design in solving energy requirements. The requirements of energy for the building depends on the partly form wind energy due to the cladding of the building that came from the surroundings of the high-rise building. In this study of the wind energy, the cladding of the building was assessed a tentative study. The wind energy obtains from several small wind powers that came from the building or the surrounding of the building. In making a cladding the wind energy forms with wind pressure by means of energy transformation methods. The assessment for the building cladding was surrounded of wind speed and wind pressure that was carried out as a result of numerical simulation of wind environment and wind pressure which is coefficient around the high-rise building with the computational fluid dynamics. In case of the obtained wind energy from the pressure of the building cladding was estimated by the simulation of CFD of the building. The wind energy at this case was calculated by energy transform methods: the wind pressure coefficients were obtained from the simulated model for wind environment using CFD as follow. The concept for the factor of $E_f$ was suggested in this study. $$C_p=\frac{P_{surface}}{0.5{\rho}V^{2ref}}$$ $$E_c=C_p{\cdot}E_f$$ Where $C_p$ is wind pressure coefficient from CFD, $E_f$ means energy transformation parameter from the principle of the conservation of energy and $E_c$ means energy from the building cladding. The other wind energy that is $E_p$ was assessed by wind power on the building or building surroundings. In this case the small wind power system was carried out for wind energy on the place with the building and it was simulated by computational fluid dynamics. Therefore the total wind energy in the building was calculated as the follows. $$E=E_c+E_p$$ The energy transformation, which is $E_f$ will need more research and estimation for various wind situation of the building. It is necessary for the assessment to make a comparative study about the wind tunnel test or full scale test.

• 국제초고층학회논문집
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• 제1권2호
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• pp.99-105
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• 2012

The higher the building height and the larger the temperature difference between the outdoor and indoor space, the more remarkable is the draft driven by the stack effect in high-rise buildings. Moreover, the stack effect can bring about the deterioration of habitability and the degradation of the performance of the indoor control system in high-rise buildings. In this study, as a measure to attenuate the stack effect, the E/V shaft cooling method was proposed and its performance was compared with the conventional stack effect control method for strengthening the air-tightness of the building using a numerical simulation method. The total decreasing ratios on the stack effect in a building were compared, and the probabilities of the secondary problems were analyzed. The results show that the E/V shaft cooling is very effective to decrease the stack effect in a high-rise building in terms of the reduction performance and application. Moreover, this method does not cause secondary problems, such as stack pressure transition to other walls, unlike the conventional stack effect mitigation method.

• Journal of Pharmaceutical Investigation
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• 제8권1호
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• pp.17-26
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• 1978

Effects of Acanthopanax EtOH Extract (AEE) on the serum total cholesterol content of normal and cholesterol administered rabbits were investigated as a series of studies on pharmacological action, especially blood pressure to Korean Acanthopanax. AEE was administered orally(100mg/kg/day) and subcutaneously (30mg/kg/day) in both normal and cholesterol administered rabbits for 36 days. In this experiment the results obtained by comparing with values of the corresponding control group were as follows; 1) In the normal rabbits, long-term administration of AEE for 36 days did not entirely influence the serum total cholesterol content measured at 12th, 24th and 36th day and also not affect the original blood pressure and changes of blood pressure to norepinephrine, angiotensin and acetylcholine recorded at 36th day. 2) In the cholesterol administered rabbits, hypercholesteremia was induced by oral administration of cholesterol(300mg/kg/day) with feed. The rise rate of serum total cholesterol content was not modified at 12th day, whereas significantly inhibited at 24th and 36th days after begining this examination in both groups orally and subcutaneously administered AEE. Original blood pressure was declined and depressor action of acetylcholine was weakened in only group admininstered orally AEE of cholesterol-fed groups. Changes of blood pressure to norepinephrine and angiotensin in these all cholesterol-fed groups, and to acetylcholine in subcutaneous group of these cholesterol-fed groups were not affected significantly by AEE.

• 한국대기환경학회지
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• 제12권3호
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• pp.279-287
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• 1996

Pressure drop and fractional collection efficiency of automotive cabin air filters were examined to obtain the basic data for the development of high performance domestic cabin air filters. Pressure drop of MA-V100 was higher than that of VF-V100, and it increased with the air flow rate. VF-V100 had longer time to rise the critical pressure drop than that MA-V100 had. Total collection efficiency of MA-V100 for initial and dust loaded conditions was higher than that of VF-V100. Also, fractional collection efficiency of MA-V100 for the fine particles was higher than that of VF-V100. Particla size distribution for the minimum collection efficiency ranged from 0.02 $\mu$m to 0.04 $\mu$m for MA-V100 and it ranged from 0.02 $\mu$m to 0.15 $\mu$m for VF-V100.

• Composites Research
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• 제24권4호
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• pp.36-40
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• 2011

본 논문은 자동차용 type II CNG 연료탱크의 손상평가를 위하여 파열시험 중 발생하는 음향방출 변수의 분석에 관한 연구이다. 음향방출 신호의 kaiser effect, felicity effect 및 creep effect의 관찰과 전체 hits에서 진폭 60dB이상의 hits가 차지하는 비율 계산으로 연료탱크의 손상도를 평가할 수 있었으며, 평균 rise time, 평균 진폭 및 평균 initial, reverbration 주파수를 분석함으로써 압력용기의 손상메커니즘을 추정하였다.

• 대한기계학회논문집B
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• 제32권2호
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• pp.83-91
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• 2008

A three-dimensional computation was conducted to understand effects of the low Reynolds number on the performance in a low-speed axial compressor at the design condition. The low Reynolds number can originates from the change of the air density because it decreases along the altitude in the troposphere. The performance of the axial compressor such as the static pressure rise was diminished by the separation on the suction surface with full span and the boundary layer on the hub, which were caused by the low Reynolds number. The total pressure loss at the low Reynolds number was found to be greater than that at the reference Reynolds number at the region from the hub to 85% span. Total pressure loss was scrutinized through three major loss categories in a subsonic axial compressor such as the profile loss, the tip leakage loss and the endwall loss using Denton#s loss model, and the effects of the low Reynolds number on the performance were analyzed in detail.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 춘계 학술대회논문집
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• pp.138-141
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• 2007

A three-dimensional computation was conducted to understand effects of the low Reynolds number on the performance in a low-speed axial compressor at the design condition. The low Reynolds number can originates from the change of the air density became it decreases along the altitude in the troposphere. The performance of the axial compressor such as the static pressure rise wag diminished by the separation on the suction surface and the boundary layer on the hub, which were caused by the low Reynolds number. The total pressure loss at the low Reynolds number was found to be greater than that at the reference Reynolds number at the region from the hub to 90% span. Total pressure loss was scrutinized through three major loss categories in a subsonic axial compressor such as profile loss, tip leakage loss and endwall loss using Denton's loss model, and effects of the low Reynolds number on the performance were analyzed in detail.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.202-212
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• 2008

A three-dimensional computation was conducted to understand effects of the low Reynolds number on the loss characteristics in a transonic axial compressor, Rotor67. As a gas turbine becomes smaller in size and it is operated at high altitude, the operating condition frequently lies at low Reynolds number. It is generally known that wall boundary layers are thickened and a large separation occurs on the blade surface in axial turbomachinery as the Reynolds number decreases. In this study, it was found that the large viscosity did not affect on the bow shock at the leading edge but significantly did on the location and the intensity of the passage shock. The passage shock moved upstream towards leading edge and its intensity decreased at the low Reynolds number. This change had large effects on the performance as well as the internal flows such as the pressure distribution on the blade surface, tip leakage flow and separation. The total pressure rise and the adiabatic efficiency decreased about 3% individually at the same normalized mass flow rate at the low Reynolds number. In order to analyze this performance drop caused by the low Reynolds number, the total pressure loss was scrutinized through major loss categories such as profile loss, tip leakage loss, endwall loss and shock loss.

• 한국추진공학회지
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• 제26권4호
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• pp.10-20
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• 2022

한국항공우주연구원의 자유제트형 지상추진시험설비인 스크램제트 엔진 시험설비의 마하 5 조건에서 스크램제트 엔진 흡입구의 성능분석 시험을 진행하였다. 스크램제트 엔진 흡입구의 대표적인 성능 인자인 전압력 회복률, 공기 포획율 측정을 위하여 격리부 후방에 설치되는 피토/정압 레이크가 설계 제작되었다. 격리부 후방에 장착된 레이크가 전방의 흡입구 램프와 격리부에 미치는 영향과 레이크로 측정된 흡입구의 성능 인자 분석 그리고 흡입구의 받음각 변화에 따른 벽면 정압력 분포 변화에 대한 분석이 수행되었다. 끝으로 연소기에서의 압력 상승을 모사하는 장치인 흡입구 후방 배압 조정 장치를 이용하여 흡입구 불시동이 발생하는 시점을 확인하였으며, 본 논문에는 그 결과를 정리하였다.