• Title/Summary/Keyword: 흡입력

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지식 한 줌 - 천 년의 금서

  • Hong, Eun-Jeong
    • 핵융합뉴스레터
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    • s.46
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    • pp.19-19
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    • 2010
  • 한국 핵융합의 획기적인 발전을 주도하며 ETER 플라즈마 제어업무를 담당했던 한 물리학자의 이야기. 비록 모든 배경이 픽션이긴 하지만 김진명 작가의 책 '천 년의 금서'는 NFRI에 소속된 나의 호기심을 자극하기 충분했다. 물론 우리나라의 왜곡된 역사를 바로잡는 과정이 책의 주 내용이고 핵융합 자체는 크게 비중을 차지하는 것이 아님에도 책에 쉽게 몰입할 수 있었던 데에는 김진명 작가 특유의 흡입력도 한몫했다.

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Effects of Aroma Blending Oil Inhalation on Academic Stress and Class Concentration in Nursing Students (아로마 블렌딩 오일 흡입이 간호대학생의 학업스트레스와 수업집중력에 미치는 영향)

  • Mi-Ae Kang
    • Journal of Internet of Things and Convergence
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    • v.9 no.2
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    • pp.33-40
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    • 2023
  • This study was aimed at examining the effects of aroma blending oil inhalation on academic stress and class concentration in nursing students. The research design was a nonequivalent placebo control group nonsynchronized. The subjects of the study were 24 students in the treatment group and 24 placebo control group. Data collection was from November 4, 2022 to December 3, 2022, and the data were analyzed chi-square test, independent t-test, paired t-test using the SPSS 23.0 Program. The treatment group inhaled aroma blending oil for 10 days showed a significant decrease in academic stress (t=-8.79, p<.001) and a significant increase in class concentration (t=24.44, p<.001).

A Study on Crack-Prevention of Pinus Rigida during Drying by Suction Treatment of Polyetylene Grycogen (PEG흡입처리에 의한 Rigida 소나무의 건조균열방지에 관한 연구)

  • Yu, Hyo-Seon;Jeong, Se-Hui
    • Korean Journal of Materials Research
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    • v.7 no.1
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    • pp.15-20
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    • 1997
  • 목재의 건조 균열방지를 위한 진공흡입기술의 새로운 목재처리방법에 대해 연구를 수행하였다. 목재의 건조균열 방지를 위해 사용된 ployetylene grycogen(PEG) 처리재들은 PEG-1540, PEG-2000, PEG-4000, PEG-10000이었으며, 진공펌프의 감압정도는 85kPa과 39kPa 이었다. 시험결과, 진공흡입처리에 의한 PEG액의 흡입은 방사단면에 걸쳐 고르게 이루워졌음을 확인 할 수 있었다. 또한 PEG의 분자량이 증가할수록 단위시간당 PEG의 분자량이 증가할수록 단위시간당 PEG의 흡입량과 처리전.후의 함수률의 차인$\Delta$ M.C 는 PEG-2000을 변곡점으로 하여 감소하였다. 그리고 리기다 소나무의 건조균열 방지를 위한 약제 흡입처리에 있어 최적의 PEG 분자량과 농도 그리고 감압력의 조건은 각각 PEG-2000과 30%(wt.)그리고 85kPa임을 알 수 있었다.

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The Gross Thrust Estimation Technique of Air-Breathing Engine (공기 흡입 엔진의 총추력 추정 기법)

  • Kim, Jeongwoo;Jung, Chihoon;Ahn, Dongchan;Lee, Kyujoon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.3
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    • pp.97-108
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    • 2018
  • It is definitely important to measure thrust during ground test when developing air-breathing engine, and in case of air-breathing engine, gross thrust should be calculated considering not only the measured thrust but also the force induced by the air flow of engine intake. Also, side thrust like yaw and pitch should be measured and analyzed using multi-component thrust measurement system. Engine performance was accurately evaluated by calculating the gross thrust of air breathing engine precisely which is analyzed from below serial procedure: labyrinth seal isolation, 1-axis gross thrust calculation, develop multi-component thrust measurement system, and side thrust analysis.

Optimal Shape of a Ramjet Intake by using a Response Surface Method (반응표면법을 이용한 램제트 엔진 흡입구 설계인자 최적화)

  • Oh, Seok-Jin;Sung, Hong-Gye
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.10
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    • pp.68-74
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    • 2005
  • Optimal shape of a typical ramjet intake is examined numerically to maximize the total pressure recovery. A response surface method is introduced to approximately predict its performance with respect to the design parameters over the each design domain. The first deflection angle of ramp, the area of inlet throat, and the diffuser angle are chosen as a design parameter. ANOVA is used to verify the trustability of the achieved response surface. The total pressure recovery of the optimum model, compared to that of the base model, is increased by 36%. The loss of viscosity through the diffuser is estimated less than 5%.

Experimental Study on the Hysteresis of Suction Stress in Unsaturated Sand (불포화 모래의 흡입응력 이력현상에 대한 실험적 연구)

  • Song, Young-Suk;Choi, Jin-Su;Kim, Gyo-Won
    • The Journal of Engineering Geology
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    • v.22 no.2
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    • pp.145-155
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    • 2012
  • The matric suction and volumetric water content of Jumunin standard sand with a relative density of 60% were measured using an Automated Soil-Water Characteristic Curve (SWCC) apparatus during both drying and wetting processes. The test time for the drying process was longer than that for the wetting process, because the flow of water is likely to be protected by air trapped in voids within the soils during the drying process. Based on the matric suction and volumetric water content, the SWCC was estimated using the model proposed by van Genuchten (1980). For the drying process, the unsaturated fitting parameters ${\alpha}$, n, and m were 0.399, 8.586, and 0.884, respectively; for the wetting process, the values were 0.548, 5.625, and 8.220, respectively. The hysteresis phenomenon occurred in the SWCCs, which means the SWCC of the drying process is not matched with the SWCC of the wetting process. Using these unsaturated parameters, we estimated the Suction Stress Characteristic Curve (SSCC), based on the relationship between suction stress and the effective degree of saturation. The suction stress showed a rapid decrease when the matric suction exceeds the Air Entry Value (AEV). Therefore, the effective stress of unsaturated soils is different from that of saturated soils when the matric suction exceeds the AEV. The suction stress of the drying process exceeds that of the wetting process for a given effective degree of saturation. The hysteresis phenomenon was also recognized in SSCCs. The hysteresis phenomenon of SSCCs arises from that of SWCCs, which is induced by the ink bottle effect and the contact angle effect. In the case of a sandy slope, the suction stress is positive and acts to enhance the slope stability as the water infiltrates the ground, but is negative when the suction stress exceeds the AEV. The results obtained for the wetting process should be applied in analyses of slope stability, because the process of water infiltration into ground is similar to the wetting process.

Comparison of Performance on Hypersonic Intakes in Off-Design Conditions Through Numerical Simulations (전산해석을 통한 탈설계점에서의 극초음속 흡입구 성능 비교)

  • Cha, Seung-Won;Roh, Tae-Seong;Lee, Hyoung Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.3
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    • pp.195-203
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    • 2019
  • Since the hypersonic intake is directly related to the overall performance of the engine, it is essential to analyze performance characteristics under various off-design conditions. In this paper, Busemann intake and conical intake with external compression were designed, and numerical simulations were performed at on/off-design conditions. Based on the results, the overall performance characteristics of two types of intake were analyzed in various Mach numbers and angle of attacks. The results showed that performance degradation of Busemann intake with truncation angle of 2 degrees was minimal. Also, the performance of Busemann intake was higher than external compression intake at various Mach numbers, however, the starting characteristics were significantly reduced with an angle of attack.

램제트 엔진 흡입구의 점성 유동장 수치계산

  • 강호철;신동신
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2002.04a
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    • pp.59-59
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    • 2002
  • 램제트 추진기관은 압축과정을 별도의 부품 없이 형상에 의해서 감속하여 연소 압력비를 얻는다. 따라서 구동 마하수와 형상에 의해 흡입과정의 압축 효율이 결정된다. 설계점은 충분한 유량을 확보 할 수 있는 유량과 충격파 각을 조절하여 전압력 손실을 줄이도록 고려되어야 한다. 또한 연소가 일어나면 연소실 압력이 배압으로 작용하고 비행시에 받음각은 변하므로 이에 따른 성능 분석도 고려 되어야 할 사항이다. 본 연구는 국내에서 실험한 형상에 대해 수치계산을 수행하여 코드의 검증과 아울러 램제트 유동장의 수치적 시뮬레이션도 설계단계에서 하나의 도구로 이용할 수 있음을 보여준다. 실험에서는 배압 조건을 얻기 위해 유동 블록키지를 유로 내에 두어 상응하는 배압을 얻었지만 본 계산에서는 압력 경계조건을 직접 사용하였다. 유동이 비정상 특성을 가지므로 시간 정확도를 이차로 가지도록 이중시간 전진법을 사용하였다. 사용한 압력비는 충격파가 카울 끝에 닿는 임계상태에 가까운 12, 13, 14에 대해 계산을 수행하였고 부스터모드로 흡입구 끝이 막혀 있다가 램제트 모드로 바뀌어 연소실 압력이 위의 압력비라고 가정할 때의 비정상 천이 과정을 계산해 보았다. 본 계산은 흡입구 부분만을 떼어놓고 적절한 가정 하에 수행되었지만 연소실 내부도 비정상 특성을 가지므로 흡입구와 연소실을 동시에 같이 계산해야한다. 추후에 전체적인 계산을 진행하기 위한 전 단계로 흡입구 계산만을 수행하여 실험과 잘 일치하는 계산 결과를 얻었고 전체 계산을 위한 연구는 진행 중에 있다.

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Optimal Design of Two-Dimensional Hypersonic Intake Geometry (2차원 극초음속 흡입구 형상 최적 설계)

  • Kim, Chae-Hyoung;Jeung, In-Seuck
    • Journal of the Korean Society of Propulsion Engineers
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    • v.18 no.6
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    • pp.1-10
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    • 2014
  • The optimal method to intuitively and systematical design hypersonic intakes is reported. In Mach 7 flow condition, the hypersonic intake model designed by theoretical approach is corrected by CFD(Computational Fluid Dynamics) analysis based on viscous flow condition, leading to the optimum hypersonic intake model. For performance comparison with CFD analysis, the double ramp intake is superior to the single ramp intake. Furthermore, in the off-design condition, the performance of the designed hypersonic intake is little degraded.

Antimicrobial Activity and Safety Test of Natural extract including Phellodendro namurense, Eucommia ulmides Oliv extracts (황벽나무, 두충나무 추출물 등을 포함한 천연 추출물의 항균력 및 안전성)

  • Noh, Daeyoung;Joe, Suehyeon;Yang, Hyunguk;Han, Donggyun;Kim, Jinhong;Kim, Donguk
    • Korean Chemical Engineering Research
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    • v.54 no.6
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    • pp.762-766
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    • 2016
  • In this study, natural extract including Phellodendro namurense, Eucommia ulmides Oliv and Prunus padus were tested for antimicrobial activity and safety. Antimicrobial activity was measured by using opportunistic microbes such as Staphylococcus aureus, Pseudomonas aeruginosa, Escherichia coli and Candida albicans. As safety test, cell viability test, single dose oral toxicity test, single dose inhalation toxicity test, repeat dose inhalation toxicity test and eye irritation test were done. From antimicrobial test, natural extract showed execellent antimicrobial activity against Staphylococcus aureus, Pseudomonas aeruginosa, Candida albicans, Escherichia coli. From 5 kinds of safety tests, toxicity was not observed. From experimental results, natural extract including Phellodendro namurense, Eucommia ulmides Oliv and Prunus padus showed superb safety and antimicrobial effect.