• Wind and Structures
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• 제36권1호
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• pp.41-60
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• 2023

The effect of cladding panel size on the size reduction factor (SRF) of extreme area-averaging wind pressure (EAWP) on the facades of a high-rise building is often ignored in previous studies. Based on wind tunnel tests, this study investigated the horizontal and vertical correlations of wind pressure on the facade claddings of square-section high-rise buildings. Then, the influencing parameters on the SRF of the EAWP on the cladding panels were analyzed, which were the panel area, panel width, panel length and building width. The results show clear regional distinctions in the correlation of wind pressures on the building facades and the rules of the horizontal and vertical correlations are remarkably different, which causes the cladding size ratio to impact the SRF significantly. Therefore, this study suggests the use of the non-dimensional comprehensive size parameter b^𝜶h^1-𝜶/B (𝜶 is the fitting parameter) determined by the cladding panel horizontal size b, cladding panel vertical size h and the building width B rather than the cladding panel area to describe the variation of the EAWP. Finally, some empirical formula for the SRF of the EAWP on the cladding of a high-rise building is proposed with the nondimensional comprehensive size parameter.

• 한국가스학회지
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• 제16권1호
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• pp.8-14
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• 2012

수소는 온실가스 배출을 저감하기 위한 미래 에너지로 고려되고 있지만, 폭발위험에 대한 문제점을 지니고 있다. 따라서 수소가 미래 에너지로 사용되기 위해서는 폭발위험에 대한 연구가 충분히 이루어져야 한다. 폭발위험은 폭발충격에 대한 이해 즉, 폭발과정에서 압력 상승속도에 대한 분석과 밀접한 관계가 있다. 본 연구에서는 폭발에 영향을 미치는 변수, 즉 연소 전후의 비열비, 화학평형상태에서 최대폭발압력, 그리고 연소속도, 이들 변수가 압력 상승속도에 미치는 영향을 살펴보았다. 화학평형상태에서 최대폭발압력과 연소속도는 압력 상승곡선에 큰 영향을 미치는 것을 알 수 있었고, 미연소 가스의 비열비는 초기압력 상승속도보다 최종압력 상승속도에 더욱 영향을 미치고, 연소가스의 비열비는 반대로 초기압력 상승속도에 더욱 큰 영향을 미치는 것을 알 수 있었다. 연소속도는 실험 데이터로부터 구하였으며 밀폐공간에서 수소가스 폭발에서는 폭연에서 폭굉으로 전이가 일어나기에는 연소속도가 매우 느림을 알 수 있었다.

• 한국강구조학회 논문집
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• 제21권3호
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• pp.289-299
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• 2009

본 연구는 각주형 저층건축물에 작용하는 지점별 풍압을 다점동시측정시스템을 이용하여 건물 폭과 깊이변화에 따른 평균풍압분포 특성에 대한 기초적인 결과를 정리한 것이다. 본 실험에서는 건물의 폭과 깊이를 변화시킨 5개의 각주형 풍압실험모형이 사용되었으며, 풍동실험은 금오공과대학교 소재 토출식 경계층풍동에서 실시하였다. 실험결과는 저층건축물의 건물 폭 및 깊이의 변화에 따른 저층건축물의 평균풍압분포 변화경향을 건축물의 풍상면, 풍측면 및 풍하면 중심으로 특성을 분석하였다. 실험결과를 토대로 저층건축물의 구조골조 설계용 풍하중을 합리적으로 산정하기 위해 필요한 새로운 풍압계수 및 간략한 약산식을 제시하였다.

• 대한기계학회논문집B
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• 제24권4호
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• pp.561-569
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• 2000

The purpose of this study is to construct a testing equipment with which several characteristics of the domestically developed swashplate type axial piston motor can be tested and to develop a software with which the data from experiment can be stored and can be applied. The results of the study are as follows; 1) The leakage flow and the torque of the motor being stopped is propotional to supply pressure and their relation can be showed by linear equations. 2) The motor movement is not smooth below 50 rpm but it moves smoothly up 170 rpm. 3) When the motor starts or stops, the pressure rise ratio effects decisively to the max. torque.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2003년도 제21회 추계학술대회 논문집
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• pp.6-10
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• 2003

Accurate description of starting transient history allows and justifies the use of small margin of safety for the engine parts, resulting in high motor mass ratio in addition to satisfying the control and guidance requirements of the vehicle. Studies have been carried out for the prediction and reduction of ignition peak and pressure-rise rate during the starting transient of solid rocket motors. Numerical studies have been carried out using a two dimensional Navier-Stokes solver. It has been inferred through the parametric studies that, in the case of solid rocket motors with uniform port, high ignition peak is observed at high spread rate and low pressure-rise rate. In the case of the port with sudden expansion configuration, high ignition peak is observed at relatively high average spread rate and high-pressure rise rate. These studies are expected to aid the designer in reducing the ignition peak by altering the propellant properties or igniter characteristics without sacrificing the motor performance.

• 한국수소및신에너지학회논문집
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• 제21권2호
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• pp.129-135
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• 2010

Homogeneous charge compression ignition (HCCI) engines have the potential to provide both diesel-like efficiency and very low emissions of nitrogen oxide (NOx) and particulate matter(PM). However, several technical issues still must be resolved before HCCI can see application. Among these, steep pressure-rise rate which leads to narrow operating range of HCCI engine continues to be a major issue. This work investigates the combination of two methods to mitigate the excessive pressure-rise rates at high power output, namely fuel stratification and Cooled exhaust-gas recirculation (Cooled EGR), after identifying the each effects to pressure-rise rate. When applying the fuel stratification to simulation, total fuelling width of 0.15 at BDC is set as a equivalent ratio difference based on the previous research. In order to simulate the effects of cooled EGR, $CO_2$ mole fraction in pre-mixture is changed ranging from 0 to 30%. DME which has a characteristic of two-stage ignition is used as a fuel.

• 대한치과기공학회지
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• 제35권2호
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• pp.127-136
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• 2013

Purpose: In order to find out the impact of changes in polymerization conditions of orthodontic acrylic resin on maximum load. Methods: While maintaining mixing ratio 3:1 of polymer and monomer in spray-on way in the production condition of polymerization temperature $25^{\circ}C$ or $37^{\circ}C$ for 10 minutes or 30 minutes of polymerization time by pressure $3kfg/cm^2$ or $6kfg/cm^2$ in the lab maintaining $25^{\circ}C$ of room temperature, the change in maximum load rise rate was tested by producing 5 acrylic resin specimens for orthodontics per group to meet the standards of $25mm{\times}2mm{\times}2mm$ and using INSTRON with the 3rd bar 2mm in diameter and parallel support bending device of $15{\pm}0.1mm$ as test equipment showing 30.00mm/min of crosshead speed, $50{\pm}16$ N/min of load ratio in the laboratory of $24^{\circ}C$ room temperature and as a result, the following results were obtained. Results: 1. When increasing pressure from $3kfg/cm^2$ to $6kfg/cm^2$, maximum load was lowered by -4.285%. 2. When increasing polymerization time from 10 minutes to 30 minutes, maximum load rose by 3.848%. 3. When increasing polymerization temperature from $27^{\circ}C$ to $37^{\circ}C$, maximum load rose by 5.854%. Conclusion: Considering the above test results that polymerization time and polymerization temperature when polymerizing acrylic resin for orthodontics according to changes in working conditions had an impact on the rate of rise of maximum load values but the rate of rise was lowered when increasing pressure from $3kfg/cm^2$ to $6kfg/cm^2$, we came to a conclusion that high pressure more than necessary does not affect the rate of rise of maximum load.

• 항공우주시스템공학회지
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• 제18권3호
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• pp.8-16
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• 2024

수소는 매우 낮은 밀도를 갖기 때문에 화석연료와 동일한 수준의 에너지량을 저장하기 위해서는 기존과 다른 저장방식이 요구된다. 수소의 밀도를 높이는 방법으로는 수소를 액화하여 저장하는 방법이 있다. 하지만, 수소의 액화온도는 -252 ℃의 극저온이기 때문에 외부 열 유입에 의해 쉽게 기화된다. 액체수소가 기화되면 탱크 내부의 압력이 증가되는 자가증압 현상을 발생하므로, 탱크 설계 시 이 상승하는 압력을 잘 예측해야 한다. 따라서, 본 논문에서는 극저온 액체수소 연료탱크의 액체수소 충전 비율에 따른 내부 압력을 예측하였다. 탱크 내부의 압력 상승을 예측하기 위하여 1차원 열역학적 모델을 적용하였다. 열전달 모델은 열 유입, 액체수소의 기화, 연료 배출에 현상이 고려되었다. 최종적으로 연료탱크 내의 액체수소의 충전 비율에 따라 압력 상승 거동과 최대 상승 압력에 큰 차이가 있음을 확인하였다.

• 한국유체기계학회 논문집
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• 제14권6호
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• pp.96-101
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• 2011

Korea Aerospace Research Institute is performing 3 stage transonic axial compressor development program. This paper introduces design step of the compressor, the performance test results and its analysis. In the fore part of the paper, aerodynamic process of the 3 stage axial compressor is presented. To satisfy both of the mass flow and pressure rise, the compressor should rotate at a high rotational speed. Therefore the transonic flow field forms in the rotor stages and it is designed with a relatively high pressure rise per stage to satisfy its design target. The compressor stage consists of 3 stages, and the bulk pressure ratio is 2.5. The first stage is burdened with the highest pressure ratio and less pressure rises occur in the following stages. Also it is designed that tip Mach number of the first rotor row does not exceed 1.3, while the maximum relative Mach number in the rotor stage is between 1.3~1.4 to increase the compressor flow coefficient. The final design has been confirmed by iterating three dimensional CFD calculations to verify design target and some design intentions. In the latter part of the paper, its performance test processes and results are presented. The performance test result shows that the overall compressor performance targets; pressure ratio and efficiency are well achieved. The stator static pressure distributions show that the blade loading is gradually increasing from the downstream of the compressor.

• 한국가스학회지
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• 제14권6호
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• pp.7-14
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• 2010

본 연구에서는 자착화특성이 다른 DME와 n-Butane을 이용하여 다양한 흡기공급방식에 따른 HCCI엔진연소에서 압력상승률의 저감특성에 대하여 조사하였다. 연소실내부의 가스압력측정, 광학측정용 엔진을 이용한 화학발광법의 측정 그리고 화학반응수치계산을 통하여 연소실내부에서 각 국소부분의 연소특성을 파악하였다. 최대압력상승률은 DME와 n-Butane의 혼합 상태에 의해 결정되어진다. DME가 성층화되고 n-Butane이 균일하게 분포되진 조건에서 가장 많이 감소되는데 두 연료가 균일한 경우에 비해서 최대압력상승률은 0.25MPa/ms 로 저감되었고 CA50도 5deg 지각되었다.