• Title/Summary/Keyword: Wind Tunnel

Search Result 1,777, Processing Time 0.026 seconds

Fine Dust Suppression by Enzyme Induced Carbonate Precipitation: Indoor Experiment and Field Application (EICP에 의한 미세먼지 억제: 실내 실험 및 현장 적용)

  • Song, Jun Young;Ha, Seong Jun;Sim, Youngjong;Jin, Kyu-Nam;Yun, Tae Sup
    • Journal of the Korean Geotechnical Society
    • /
    • v.35 no.10
    • /
    • pp.67-78
    • /
    • 2019
  • The efficiency of suppressing fine dust was evaluated by conducting indoor and field experiments for the ground treated with EICP solution, which is an eco-friendly ground improvement method. In laboratory experiments, the EICP solution was prepared with inexpensive materials for the field applicability, and the optimal mixing ratio and optimal spraying volume of EICP solution were calculated. The optimum amount of calcium carbonate was shown when the ratio of urea/calcium chloride and white powder were 1.5 and 15 g/L, respectively. The optimum spraying amount of the EICP solution was $7L/m^2$ determined by fine dust suppression and cone tip resistance experiments. The spraying of water and EICP solution was conducted at the test-bed where dump trucks pass for the effect of suppressing fine dust of each method. The effective fine dust suppression method can be chosen depending on the situation of the site.

Comparative Study of Tip Clearance Loss in Impulse and Reaction Turbine Cascades (충동터빈과 반동터빈 캐스케이드에서의 팁 간극 손실에 대한 비교 연구)

  • Park, Kyung-Wook;Jung, Eun-Hwan;Song, Seung-Jin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2008.11a
    • /
    • pp.145-148
    • /
    • 2008
  • Korea Aeronautics Research Institute (KARI) is developing a turbo pump that has 1-stage impulse turbine and relatively high tip clearance for safety. The objective of this research is to investigate the effect of reaction on tip clearance loss in axial turbines. Both cascades were tested in a subsonic wind tunnel. In each cascade, total pressure was measured for tip clearance ranging from 1% to 20% of chord. In results, increasing tip clearance, total pressure loss in reaction turbines is continually increased but impulse turbines keep almost same level of mass averaged total pressure loss. When tip clearance becomes more than 10% of chord, mass-averaged total pressure loss in impulse turbines is less than in reaction. This means that when tip clearance is more than 10% of chord, impulse turbines have better efficiency than reaction turbines.

  • PDF

Wave Drag Reduction due to Repetitive Laser Pulses (반복 레이저 펄스를 이용한 초음속 비행체의 항력저감)

  • Kim, Jae-Hyung;Sasoh, Akihiro;Kim, Heuy-Dong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2011.04a
    • /
    • pp.381-384
    • /
    • 2011
  • Wave drag reduction due to the repetitive laser induced energy deposition over a flat-nosed cylinder is experimentally conducted in this study. Irradiated laser pulses are focused by a convex lens installed in side of the in-draft wind tunnel of Mach 1.94. The maximum frequency of the energy deposition is limited up to 80. Time-averaged drag force is measured using a low friction piston which was backed by a load cell in a cavity as a controlled pressure. Stagnation pressure history, which is measured at the nose of the model, is synchronized with corresponding sequential schlieren images. With cylinder model, amount of drag reduction is linearly increased with input laser power. The power gain only depends upon the pulse energy. A drag reduction about 21% which corresponds to power gain of energy deposition of approximately 10 was obtained.

  • PDF

Simplified Collision Analysis Method for Submerged Floating Railway Using the Theory of a Beam with an Elastic Foundation (탄성지지 보이론을 이용한 해중철도 간이 충돌해석법)

  • Seo, Sung-Il;Kim, Jin Sung
    • Journal of the Korean Society for Railway
    • /
    • v.16 no.3
    • /
    • pp.202-206
    • /
    • 2013
  • A submerged floating railway is an innovative tunnel infrastructure passing through the deep sea independent of wave and wind so that high speed trains can run on it. It doesn't depend on water depth and is cost effective due to modular construction on land. The construction period can be reduced drastically. This paper introduces the concept design of a submerged floating railway, and for securing safety, proposes a method to analyze the structural behavior of the body in case of collision with a submarine. The theory of a beam with an elastic foundation was used to calculate the equivalent mass of the body so that the perfect elastic collision could be applied to calculate the collision velocity. The maximum deformation and bending moment was analyzed based on energy conservation. To verify the results, a collision analysis using a finite element analysis code was made. Comparing the results confirmed that this simplified collision analysis method gives enough accurate deformation and bending moment to be used for actual estimation in the initial design stage.

Evaluation of Optical Porosity of Thuja occidentalis by Image Analysis and Correlation with Aerodynamic Coefficients (이미지 분석을 통한 서양측백나무의 광학적 공극도 산정 및 공기역학계수와의 상관성 평가)

  • Jang, Dong-hwa;Yang, Ka-Young;Kim, Jong-bok;Kwon, Kyeong-seok;Ha, Taehwan
    • Journal of The Korean Society of Agricultural Engineers
    • /
    • v.63 no.6
    • /
    • pp.39-47
    • /
    • 2021
  • Reduction effect of the spread of odorant and fine dust through windbreak trees can be predicted through numerical analysis. However, there is a disadvantage that a large space and destructive experiments must be carried out each time to calculate the aerodynamic coefficient of the tree. In order to overcome these shortcomings, In this study, we aimed to estimate the aerodynamic coefficient (C0, C1, C2) by using image processing. Thuja occidentalis, which can be used as windbreak were used as the material. The leaf area index was estimated from the leaf area ratio using image processing with leaf weight, and the optical porosity was calculated through image processing of photos taken from the side while removing the leaves step-by-step. Correlation analysis was conducted with the aerodynamic coefficient of Thuja occidentalis calculated from the wind tunnel test and leaf area index and optical porosity calculated from the image analysis. The aerodynamic coefficient showed positive and negative correlations with the leaf area index and optical porosity, respectively. The results showed that the possibility of estimating the aerodynamic coefficient using image processing.

Application of Chemical Dust Suppressants for Control of Fugitive Dust in Ash pond of Thermal Power Plant (화력발전소의 회처리장 내 비산먼지 저감을 위한 화학적 먼지억제제 적용 연구)

  • Choi, Yu-Lim;Choi, Jong-Soo;Yang, Jae-Kyu;Park, Sun-Hwan;Joo, Hyun Soo;Chang, Yoon-Young
    • Journal of Soil and Groundwater Environment
    • /
    • v.23 no.6
    • /
    • pp.82-89
    • /
    • 2018
  • The objective of this study is to evaluate efficiencies of chemical suppressants for control of fugitive dust in ash pond of thermal power plant. In this study, $MgCl_2$, PAM (polyacrylamide), and PVA (poly vinyl alcohol) that are generally applied to suppression of fugitive dust generated from unpaved road, coal mining, storage piles and etc, were employed as chemical dust suppressants. The coal ash (coal combustion residuals) were sampled from the ash pond of Yeongheung power division in Incheon, South Korea. The characterization of the sample including particle size distribution, pH, $pH_{PZC}$ and pore volume as well as XRF analysis were carried out. The suppressant treated-samples were investigated with the wind tunnel experiments to estimate and compare the effect of suppressants on stabilization of the surface of coal ash samples. According to the results, the stability of suppressant-treated samples were significantly improved compared to water-treated samples. Among the three kinds of suppressants, PAM and PVA showed higher efficiencies and cost saving than $MgCl_2$.

Computational Modeling and Analysis of Ablative Composites Using Micro-tomographic Images (미세 단층 영상을 이용한 삭마 복합재료의 전산 모델링 및 해석)

  • Cheon, Jae Hee;Roh, Kyung Uk;Shin, Eui Sup
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.47 no.9
    • /
    • pp.642-648
    • /
    • 2019
  • In this study, Image-based computational analysis using the developed models was performed to predict the degradation of effective properties by ablation. The ablation tests of carbon/phenolic composites were performed using a 0.4 MW arc-heated wind tunnel. The carbon/phenolic composite samples were scanned using the micro-computed tomography (Micro-CT) to analyze the ablation characteristics according to a duration time of the ablation test. By calibrating the scanned images, computational models were developed that reflect the actual microstructure of the ablation composites. Also, nine computational models that reflect the actual pore shape were developed using the created cross-sectional images. Image-based computational analysis using the developed models was performed to predict the degradation of effective properties by ablation and the decrease of effective properties was confirmed with increase of porosity.

Thermomechanical Coupled Analysis of Carbon/phenolic Composite Structures in Reentry Environments (재진입 환경의 탄소/페놀릭 복합재 구조물의 열기계적 연계 해석)

  • Son, Myeong Jin;Shin, Eui Sup
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.47 no.6
    • /
    • pp.414-421
    • /
    • 2019
  • In this paper, thermomechanical coupled analysis of carbon/phenolic composites structures in reentry environment was performed. The interface of thermomechanical coupled analysis was constructed using commercial software. The governing equations of temperature and displacement fields were considered to simulate change of physical behavior due to pyrolysis and ablation effects. The results of thermomechanical coupled analysis were compared with the results of ablation test using arc-heated wind tunnel. Also, the structural stability of reentry capsule was analyzed using the analysis interface. The excellent ablation characteristics and thermal protection effects of the carbon/phenolic composites were confirmed and the constructed analysis interface can be effectively used to perform thermal protection system design.

Indirect Verification of the Icing Test Condition Using Ice Thickness (얼음두께를 이용한 결빙시험조건의 간접 확인기법)

  • Kim, Yoo Kyung;Park, Nameun;Choi, Gio
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.46 no.11
    • /
    • pp.944-951
    • /
    • 2018
  • Artificial icing test and wind tunnel test can be performed to reduce the development period when a rotorcraft is required operation under icing situations. Artificial icing test of the KUH(Korean Utility Helicopter) was performed in advance to verify anti-icing and de-icing performance before natural icing test. Although high-precision sensor, the CCP(Cloud Combination Probe) is used to measure icing test condition parameters such as LWC(Liquid Water Content) and MVD(Median Volume Diameter), the measured values need to be verified in various methods due to the possibility of uncertainties which are the test atmosphere environment, sensor errors, and etc. The calculated LWC from the ice thickness cumulated on the fuselage of the KUH is compared to the measured value by CCP, and the results show the effective indirect method to check the test conditions.

Aerodynamic Analysis Based on the Truncation Ratio of Guided-Weapon Nose Using CFD (전산유체역학을 이용한 유도무기 선두부 절단 비율에 대한 공력해석)

  • Jeong, Kiyeon;Kang, Dong-Gi;Lee, Daeyeon;Noh, Gyeongho
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.47 no.4
    • /
    • pp.245-255
    • /
    • 2019
  • This paper describes on aerodynamic analysis based on the truncation rate of guided-weapon nose using computational fluid dynamics. The shape to perform the analysis is only the body of the guided weapon and the diameter to length ratio is 10.7. Three nose shapes were selected and hemisphere, 25% and 50% truncation were compared. For the accurate CFD analysis of the body, the grid method and the analytical method were selected and verified using NASA wind tunnel test data. For the three nose shapes, the drag analysis for the flight Mach number is 6~20% different. This difference was analyzed by the pressure distribution from nose to base.