59 research outputs found

    Trinitrobenzene sulfonic acid๋กœ ์œ ๋„ํ•œ ๋Œ€์žฅ์—ผ์—์„œ ๋Œ€์žฅํ†ต๊ณผ์‹œ๊ฐ„ ๋ณ€ํ™” ๋ฐ ์žฅ๋ฒฝ๋‚ด nitric oxide synthase์˜ ๋ถ„ํฌ

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    ์˜ํ•™๊ณผ/์„์‚ฌ[ํ•œ๊ธ€] Nitric oxide (NO)๋Š” ๋Œ€์žฅ์—์„œ ์—ฐ๋™ ๋ฐ˜์‚ฌ์‹œ ๋ฏธ์ธก ์œค์ƒ๊ทผ์˜ ์ด์™„์— ๊ด€์—ฌํ•˜๋Š” ๋ฌผ์งˆ๋กœ์„œ, ์ •์ƒ์ ์ธ ์ƒ๋ฆฌ์กฐ๊ฑด์—์„œ๋Š” endothelial nitric oxide synthase (eNOS) ๋ฐ neuronal NOS (nNOS)์— ์˜ํ•ด ์ฃผ๋กœ ์ƒ์„ฑ๋˜๋ฉฐ, ๋Œ€์žฅ์—ผ์‹œ์—๋Š” ๋‹ค์–‘ํ•œ ์—ผ์ฆ์„ธํฌ๋กœ๋ถ€ํ„ฐ ํ•ฉ์„ฑ๋œ inducible NOS (iNOS)์— ์˜ํ•ด ์ƒ์„ฑ๋˜๋Š” ๊ฒƒ์œผ๋กœ ์•Œ๋ ค์ ธ ์žˆ๋‹ค. ์ตœ๊ทผ ๋ฐ• ๋“ฑ์€ trinitrobenzene sulfonic acid (TNBS) ์œ ๋„ ๊ธฐ๋‹ˆ ํ”ฝ ๋Œ€์žฅ์—ผ ๋ชจ๋ธ์—์„œ ๋Œ€์žฅํ†ต๊ณผ ์‹œ๊ฐ„์€ ์•ฝ์ œ ์ฃผ์ž… ํ›„ 3์ผ์งธ๋ถ€ํ„ฐ ์œ ์˜ํ•˜๊ฒŒ ์ง€์—ฐ๋˜์ง€๋งŒ ์—ผ์ฆ์˜ ์ •๋„์™€ ์ƒ๊ด€ ๊ด€๊ณ„๋ฅผ ๋ณด์ด์ง€ ์•Š์œผ๋ฉฐ, ๋ฌด์Šค์นด๋ฆฐ์„ฑ ์ˆ˜์šฉ์ฒด๋ฅผ ํ†ตํ•œ ํ‰ํ™œ๊ทผ ์„ธํฌ์˜ ์ˆ˜์ถ• ๋ฐ˜์‘์—๋Š” ์ด์ƒ์ด ์—†์Œ์„ ๋ณด๊ณ ํ•˜์˜€๋‹ค. ๋ณธ ์—ฐ๊ตฌ์—์„œ๋Š” ๊ธฐ๋‹ˆ ํ”ฝ์—๊ฒŒ TNBS๋กœ ์œ ๋„ํ•œ ์‹คํ—˜์  ๋Œ€์žฅ์—ผ ๋ชจ๋ธ์—์„œ ๋Œ€์žฅํ†ต๊ณผ์‹œ๊ฐ„์˜ ๋ณ€ํ™” ์—ฌ๋ถ€๋ฅผ ๊ด€์ฐฐํ•˜๊ณ , TNBS ๋…ธ์ถœ ๊ธฐ๊ฐ„์— ๋”ฐ๋ฅธ nNOS์™€ iNOS์˜ ์žฅ๋ฒฝ๋‚ด ๋ถ„ํฌ๋ฅผ ์กฐ์‚ฌํ•˜์—ฌ ๋Œ€์žฅํ†ต๊ณผ์‹œ๊ฐ„ ๋ณ€ํ™”์™€ ๋‹ˆํŠธ๋ ˆ์ง(nitrergic) ์‹ ๊ฒฝ๋ถ„ํฌ์™€์˜ ์ƒ๊ด€ ๊ด€๊ณ„๋ฅผ ์•Œ์•„๋ณด๊ณ ์ž ํ•˜์˜€๋‹ค. ์‹คํ—˜ ๊ฒฐ๊ณผ, ๋Œ€์žฅํ†ต๊ณผ์‹œ๊ฐ„์€ TNBS ํˆฌ์—ฌ๊ตฐ์—์„œ 3, 7, 14์ผ ์งธ์— ๋Œ€์กฐ๊ตฐ์— ๋น„ํ•˜์—ฌ ์œ ์˜ํ•˜๊ฒŒ ์ง€์—ฐ๋˜๋Š” ๊ฒƒ์„ ๊ด€์ฐฐํ•˜์˜€๋‹ค. nNOS ์–‘์„ฑ ์„ธํฌ๋Š” ๋Œ€์กฐ๊ตฐ์—์„œ ์ ๋ง‰, ์ ๋ง‰ํ•˜์ธต, ๊ณ ์œ ๊ทผ์ธต, ์ ๋ง‰ํ•˜ ์‹ ๊ฒฝ์ด, ๊ทธ๋ฆฌ๊ณ  ์žฅ๊ทผ ์‹ ๊ฒฝ์ด์—์„œ ๊ณจ๊ณ ๋ฃจ ๊ด€์ฐฐ๋˜์—ˆ๋‹ค. TNBS ์ฃผ์ž…๊ตฐ์—์„œ๋Š” ์ฃผ๋กœ ์—ผ์ฆ์ด ์œ ๋ฐœ๋œ ์ ๋ง‰ ๋ฐ ์ ๋ง‰ํ•˜์ธต์—์„œ nNOS ์–‘์„ฑ ์„ธํฌ์˜ ๊ฐ์†Œ๊ฐ€ ๊ด€์ฐฐ๋˜์—ˆ์œผ๋‚˜, ๊ฐ ๊ตฐ์—์„œ ์žฅ๊ทผ ์‹ ๊ฒฝ์ด์˜ nNOS ์–‘์„ฑ ์‹ ๊ฒฝ์„ธํฌ์˜ ์ˆ˜๋Š” ์œ ์˜ํ•œ ์ฐจ์ด๋ฅผ ๋ณด์ด์ง€ ์•Š์•˜๋‹ค. iNOS ์–‘์„ฑ ์„ธํฌ๋Š” ๋Œ€์กฐ๊ตฐ์—์„œ ์ฃผ๋กœ ์ ๋ง‰ํ•˜ ์‹ ๊ฒฝ์ด ๋ฐ ์žฅ๊ทผ ์‹ ๊ฒฝ์ด์—์„œ ๊ด€์ฐฐ๋˜์—ˆ๋‹ค. TNBS ์ฃผ์ž…๊ตฐ์—์„œ๋Š” ์ฃผ๋กœ ์—ผ์ฆ์ด ์œ ๋ฐœ๋œ ์ ๋ง‰ ๋ฐ ์ ๋ง‰ํ•˜์ธต์—์„œ iNOS ์–‘์„ฑ ์„ธํฌ์˜ ์ฆ๊ฐ€๊ฐ€ ๊ด€์ฐฐ๋˜์—ˆ์œผ๋‚˜ TNBS ๋…ธ์ถœ๊ธฐ๊ฐ„์— ๋”ฐ๋ฅธ ๋ณ€ํ™”๋Š” ๊ด€์ฐฐ๋˜์ง€ ์•Š์•˜์œผ๋ฉฐ, ๊ฐ ๊ตฐ์—์„œ ์žฅ๊ทผ ์‹ ๊ฒฝ์ด ๋‚ด iNOS ์–‘์„ฑ ์„ธํฌ์˜ ์ˆ˜๋Š” ์œ ์˜ํ•œ ์ฐจ์ด๋ฅผ ๋ณด์ด์ง€ ์•Š์•˜๋‹ค. ๊ฒฐ๋ก ์ ์œผ๋กœ TNBS ์œ ๋„ ๊ธฐ๋‹ˆ ํ”ฝ ๋Œ€์žฅ์—ผ์—์„œ ๋Œ€์žฅํ†ต๊ณผ์‹œ๊ฐ„์ด ์œ ์˜ํ•˜๊ฒŒ ์ง€์—ฐ๋˜์—ˆ์œผ๋ฉฐ, ์žฅ๊ทผ ์‹ ๊ฒฝ์ด๋‚ด nNOS์™€ iNOS ์–‘์„ฑ ์„ธํฌ์˜ ๋ถ„ํฌ๋ณ€ํ™”๋Š” ๋Œ€์žฅํ†ต๊ณผ์‹œ๊ฐ„ ๋ณ€ํ™”์— ์ฃผ ์—ญํ• ์„ ํ•˜์ง€ ์•Š๋Š” ๊ฒƒ์œผ๋กœ ์ƒ๊ฐ๋œ๋‹ค. [์˜๋ฌธ]Inflammation-induced alterations in smooth muscle contractility may be due to effects on smooth muscle itself, or its response to neurotransmitters or to effects on enteric nerves. Colonic transit in trinitrobenzene sulfonic acid (TNBS)-induced colitis of guinea pigs is delayed significantly, but it is not related to the muscarinic receptor-mediated contractions. In dextran sulfate sodium-induced colitic rat, the delay in colon-ic transit was caused by decreased activity and production of neuronal nitric oxide synthase (nNOS) in the myenteric plexus in the distal colon. In this study, we investigated the distribution of inducible NOS/(iNOS) and nNOS immunoreactive cells in the myenteric plexus and colonic wall to explain the involvement of NOS in delayed colonic transit in TNBS-induced colitic guinea pig. Colonic transit was delayed significantly at 3, 7 and 14 days after administration of TNBS compared to control. In control, nNOS immunoreactivity was present in the mucosa, submucosa, lamina propria, muscularis mucosa, and in ganglion cells within the myenteric plexus, while after TNBS, reduced nNOS cells were found. However, the number of nNOS immunoreactive ganglion cells in the myenteric plexus was similar to that seen in controls. After administration of TNBS, iNOS immunoreactivity was increased in the mucosa and submucosa compared to that in control, but the number of distribution of iNOS immunoreactive ganglion cells in the myenteric plexus was not changed compared to that in control. In conclusion, it is suggested that in TNBS-induced guinea pig colitis, delayed colonic transit is not associated with the expression of nNOS or iNOS in the myenteric plexus.ope

    Correlation between Clinical Symptoms and Radiologic Findings before and after Pneumatic Balloon Dilatation for Achalasia

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    Background/Aims: We investigated the risk factors for short-term recurrence and analyzed the correlation between subjective clinical symtoms and objective radiological findings in patients with achalasia undergoing pneumatic balloon dilatation. Methods: Twenty patients who were treated by pneumatic balloon dilatation were enrolled. We compared prospectively various indices before and after the treatment as follows: 1) Eckardt symptom score and dysphagia grade, 2) The ratio of the maximal width in mid-esophageal lumen to the minimal width in distal esophagus around lower esophageal sphincter, and 3) the percentage of maximum activity retained in the esophagus at 30 seconds and Tยฝ in esophageal scan two days after the treatment. Results: 1) Clinical indices and radiologic indices significantly improved after pneumatic dilatation. 2) There was no significant correlation between the clinical indices and the radiologic indices before and after the treatment. 3) The difference percentage of clinical indices did not show significant correlation with the difference percentage of the radiologic indices. 4) Compared to the group above 20% in the difference percentage of 30 second residual fraction, the one below 20% had a four-fold risk in short-term recurrence. Conclusions: Clinical symptoms and radiologic indices significantly improve after pneumatic dilatation but have no significant correlation to each other. The group below 20% in the difference percentage of 30 second residual fraction has a high risk of recurrence and may need careful examination and early repeated pneumatic dilationope

    ๋งˆ๊ทธ๋„คํ† ์ŠคํŠธ๋ฆญ์…˜ ํšจ๊ณผ๋ฅผ ์ด์šฉํ•œ ๋น„์ ‘์ด‰ ๋ชจ๋‹ฌ ํ…Œ์ŠคํŒ… ๊ธฐ๋ฒ•

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    Thesis (master`s)--์„œ์šธ๋Œ€ํ•™๊ต ๋Œ€ํ•™์› :๊ธฐ๊ณ„ํ•ญ๊ณต๊ณตํ•™๋ถ€,2001.Maste

    ๊ทน์ €์ฃผํŒŒ์— ์˜ํ•œ ๊ฐ€๋Œ๋ฆฌ๋Š„์˜ ์„ธํฌ์œ ์ „๋…์„ฑ ์ฆ์ง„ํšจ๊ณผ

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    Gadolinium (Gd) is widely used for various industrial and medical purposes, particularly in magnetic resonance imaging (MRI) contrast agent. As there has been a large volume of studies about cyto- and geno- toxicity of Gd, it has been utilized as derivatives by chelation with various ligands. Human exposure to Gd and its derivatives is significantly increasing, posing a high risk of accumulation and retention. It is important to investigate the effect of extremely low-frequency electromagnetic fields (ELF-EMF) on the cyto- and geno-toxicity of Gd, since patients are co-exposed to Gd and ELF-EMF generated by MRI scanner. The aim of this study is to investigate the cyto- and geno-toixcity of Gd and the possible enhancing effect of ELF-EMF on the toxicity of Gd in cultured human peripheral blood lymphocytes by performing micronuclei (MN) assay, single cell gel electrophoresis (Comet) assay, trypan blue dye-exclusion assay, apoptosis analysis using flow cytometry and intracellular reactive oxygen species measurement. MN frequencies were 13.0, 14.0, 15.3 and 17.7 per 1000 cells in Gd treatment cells at concentrations of 0, 0.4, 0.8 and 1.2 mM. ELF-EMF exposure (0.8 mT) increased the frequencies of MN induced by Gd treatment alone; 13.3, 17.0, 20.3 and 25.0 per 1000 cells at each Gd concentrations. ELF-EMF exposure also increased cell death, olive tail moment (OTM), apoptosis and ROS level induced by Gd treatment alone. These results suggest that Gd induces DNA damage, apoptotic cell death and ROS generation in human lymphocytes and ELF-EMF can enhance the cyto- and geno-toxicity of Gd.1. Introduction 1 2. Materials & Methods 4 2. 1. Isolation, culturing and stimulation of peripheral blood lymphocytes 5 2. 2. Gd treatment and ELF-EMF exposure condition 5 2. 3. Measurement of cell death 6 2. 4. Cytokinesis-block micronuclei (CBMN) assay 6 2. 5. Single-cell gel electrophoresis (comet) assay 7 2. 6. Detection and quantification of apoptosis 8 2. 7. Measurement of intracellular ROS 9 2. 8. Statistical analysis 10 3. Results 10 3. 1. ELF-EMF enhances Gd-induced cell death in peripheral blood lymphocytes 11 3. 2. ELF-EMF enhances Gd-induced micronuclei in peripheral blood lymphocytes 13 3. 3. ELF-EMF enhances Gd-induced DNA damage in peripheral blood lymphocytes 15 3. 4. ELF-EMF enhances Gd-induced apoptosis in peripheral blood lymphocytes 17 3. 5. ELF-EMF enhances the generation of ROS induced by Gd 19 4. Discussion 23 5. Conclusion 30 6. Reference 31Maste

    ์ž๊ธฐ๋ณ€ํ˜•์„ ์ด์šฉํ•œ ์œ ๋„์ดˆ์ŒํŒŒ ๋ฐ ์ง„๋™ ํŠธ๋žœ์Šค๋“€์„œ์˜ ์„ค๊ณ„

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    Thesis(doctoral)--์„œ์šธ๋Œ€ํ•™๊ต ๋Œ€ํ•™์› :๊ธฐ๊ณ„ํ•ญ๊ณต๊ณตํ•™๋ถ€,2006.Docto

    ๋Œ€ํ™”ํ˜• ์œ ์ „ ์•Œ๊ณ ๋ฆฌ์ฆ˜์„ ์ด์šฉํ•œ ์ด๋ฏธ์ง€ ์ƒ‰ ์–‘์žํ™”

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    ํ•™์œ„๋…ผ๋ฌธ (์„์‚ฌ)-- ์„œ์šธ๋Œ€ํ•™๊ต ๋Œ€ํ•™์› : ์ „๊ธฐยท์ปดํ“จํ„ฐ๊ณตํ•™๋ถ€, 2015. 2. ๋ฌธ๋ณ‘๋กœ.Color image quantization is the problem of converting the given image to the image with limited number of colors used, maximizing the similarity. Previous studies measured the similarity as the smaller color difference by pixels, which is hard to evaluate the context of the image. In this thesis, a novel approach of considering the context is shown. Interactive genetic algorithm is applied to reflect the human knowledge in generating the quantized images. The experiment of the system has been done with 12 subjects and four test images, and the result shows that the quantized images generated with the interactive system are evaluated to be more suitable than those with the traditional optimization methods.Abstract i Contents ii List of Figures iv List of Tables v Chapter 1 Introduction 1 Chapter 2 Preliminaries 4 2.1 Color Image Quantization Problem 4 2.2 Genetic Algorithm 5 2.3 Hybrid Genetic Algorithm 8 2.4 Interactive Genetic Algorithm 9 Chapter 3 The Proposed System 11 3.1 Formulation of the Problem 11 3.2 The Framework of the System 11 3.3 The Structure of Chromosomes 14 3.4 Interactive Step and Evolutionary Step 15 3.5 Measurement of Fitness 17 3.6 Local Optimization 17 Chapter 4 Experiment 19 4.1 Experimental Setup 19 4.2 Generated Image 20 4.3 Comparison of Results 21 Chapter 5 Conclusion 24 ์š”์•ฝ 28Maste

    NudH์— ์˜ํ•œ ๋Œ€์žฅ๊ท  ์งˆ์†Œ์ธ์‚ฐ์ „๋‹ฌ๊ณ„์˜ ์ธ์‚ฐํ™” ๋ฐ ?S ์˜ ํ™œ์„ฑ ์–ต์ œ

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    Thesis(doctors) --์„œ์šธ๋Œ€ํ•™๊ต ๋Œ€ํ•™์› :์ƒ๋ช…๊ณผํ•™๋ถ€, 2009.2.Docto

    ์ข…๋ฐฉํ–ฅ ์ŠคํŠธ๋ฆฝ์„ ์ด์šฉํ•œ ๋‚ฎ์€ ๋ ˆ์ด๋†€์ฆˆ ์ˆ˜ ์ตํ˜• ์ฃผ๋ณ€ ์œ ๋™ ์ œ์–ด

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    ํ•™์œ„๋…ผ๋ฌธ (๋ฐ•์‚ฌ)-- ์„œ์šธ๋Œ€ํ•™๊ต ๋Œ€ํ•™์› : ๊ณต๊ณผ๋Œ€ํ•™ ๊ธฐ๊ณ„ํ•ญ๊ณต๊ณตํ•™๋ถ€, 2019. 2. ์ตœํ•ด์ฒœ.๋ณธ ์—ฐ๊ตฌ์—์„œ ์ข…๋ฐฉํ–ฅ ์ŠคํŠธ๋ฆฝ์„ ์ตํ˜•์˜ ํ‘œ๋ฉด์— ์„ค์น˜ํ•˜์—ฌ ์‹ค์†์„ ์ œ์–ดํ•˜์˜€๋‹ค. ์ข…๋ฐฉํ–ฅ ์ŠคํŠธ๋ฆฝ์— ์˜ํ•œ ์‹ค์† ์ง€์—ฐ๊ณผ ์œ ๋™ ์ œ์–ด ๋ฉ”์ปค๋‹ˆ์ฆ˜์„ ์‹คํ—˜์ ์œผ๋กœ ๊ทœ๋ช…ํ•˜์˜€๋‹ค. ์ตํ˜•์€ SD7003์ด๋ฉฐ, ์ž์œ ๋ฅ˜ ์†๋„์™€ ์ตํ˜• ์ฝ”๋“œ ๊ธธ์ด๋ฅผ ๊ธฐ์ค€์œผ๋กœ ํ•˜๋Š” ๋ ˆ์ด๋†€์ฆˆ ์ˆ˜๋Š” 60,000๊ณผ 180,000์ด๋‹ค. ์ŠคํŠธ๋ฆฝ์ด ์žˆ๋Š” ๊ฒฝ์šฐ์™€ ์—†๋Š” ๊ฒฝ์šฐ ๊ฐ๊ฐ์— ๋Œ€ํ•ด ๋ฐ›์Œ๊ฐ์„ 0ยฐ์—์„œ 16ยฐ ๊นŒ์ง€ ๋ณ€ํ™”์‹œํ‚ค๋ฉฐ ์–‘๋ ฅ๊ณผ ํ•ญ๋ ฅ์„ ์ง์ ‘ ์ธก์ •ํ•˜์˜€๋‹ค. ์ŠคํŠธ๋ฆฝ์˜ ์ตœ์  ํ˜•์ƒ์€ ๋ฐ˜์‘ํ‘œ๋ฉด๋ฒ•(Response surface method)์— ์˜ํ•ด ์–ป์–ด์กŒ๋‹ค. ์ŠคํŠธ๋ฆฝ์ด ์—†๋Š” ๊ฒฝ์šฐ์—, ๋ ˆ์ด๋†€์ฆˆ 60,000๊ณผ 180,000์—์„œ ๊ธ‰๊ฒฉํ•œ ์‹ค์†์ด ๊ฐ๊ฐ 11ยฐ์™€ 13ยฐ์—์„œ ์ผ์–ด๋‚ฌ๋‹ค. ๋ฐ˜๋ฉด, ์ตœ์  ํ˜•์ƒ์„ ๊ฐ–๋Š” strip์ด ์„ค์น˜๋˜์—ˆ์„ ๋•Œ ์ด๋Ÿฌํ•œ ๊ธ‰๊ฒฉํ•œ ์‹ค์†์ด ๋ฐœ์ƒ๋˜์ง€ ์•Š๋Š”๋‹ค. ์ด๋Ÿฌํ•œ ์ŠคํŠธ๋ฆฝ์— ์˜ํ•ด ์‹ค์† ์ดํ›„ ์–‘๋ ฅ ๊ณ„์ˆ˜๋Š” ํ˜„์ €ํžˆ ์ฆ๊ฐ€๋˜์—ˆ์œผ๋ฉฐ, ํ•ญ๋ ฅ ๊ณ„์ˆ˜๋Š” ๊ฐ์†Œ๋˜์—ˆ๋‹ค. ์ฝ”๋„ˆ ๋ณผํ…์Šค๊ฐ€ ์ตํ˜•์˜ ์„ ๋‹จ ๋ถ€๊ทผ์˜ strip์˜ ์–‘ ์ฝ”๋„ˆ์—์„œ ๋ฐœ์ƒํ•จ์„ ํ™•์ธํ•˜์˜€๋‹ค. ์‹œ๊ณ„๋ฐฉํ–ฅ ๋ฐ ๋ฐ˜์‹œ๊ณ„ ๋ฐฉํ–ฅ์˜ ์œ ์„ ํ˜• ๋ณผํ…์Šค๊ฐ€ ๊ฐ๊ฐ ์ŠคํŠธ๋ฆฝ์˜ ์™ผ์ชฝ ๋ฐ ์˜ค๋ฅธ์ชฝ ์ฝ”๋„ˆ์—์„œ ๋ฐœ์ƒํ•˜์˜€์œผ๋ฉฐ, ์ด๋Š” ํ•˜๋ฅ˜๋กœ ์ด๋™ํ•จ์— ๋”ฐ๋ผ ์ ์ฐจ ๋ชจ์„œ๋ฆฌ์—์„œ ๋ฉ€์–ด์ง€๊ฒŒ ๋œ๋‹ค. ์ด๋Ÿฌํ•œ ๋ณผํ…์Šค๋“ค์€ ์ตํ˜•์˜ ํก์ž…๋ฉด์— ์ถ”๊ฐ€์ ์ธ ๋ชจ๋ฉ˜ํ…€์„ ๊ณต๊ธ‰ํ•˜์—ฌ ๊ฒฐ๊ณผ์ ์œผ๋กœ ์ŠคํŠธ๋ฆฝ์—์„œ์˜ ๋ถ€์ฐฉ์œ ๋™์„ ์œ ์ง€ํ•˜๊ฒŒ ํ•จ๊ณผ ๋™์‹œ์— ์ตํ˜• ์œ„์—์„œ์˜ ์„ ๋‹จ ์œ ๋™ ๋ฐ•๋ฆฌ๋ฅผ ์žฌ๋ถ€์ฐฉ์‹œํ‚ค๊ฒŒ ๋œ๋‹ค. ์ด๋Ÿฌํ•œ ์ข…๋ฐฉํ–ฅ ์ŠคํŠธ๋ฆฝ์€ ์ด์ „์˜ ๋‚ฎ์€ ๋ ˆ์ด๋†€์ฆˆ ์ˆ˜ ์กฐ๊ฑด์—์„œ ์‹ค์†์„ ์ œ์–ดํ•˜๊ธฐ ์œ„ํ•œ ์ œ์–ด์žฅ์น˜์ธ ์™€๋ฅ˜ ๋ฐœ์ƒ๊ธฐ๋‚˜, ํŠธ๋ฆฝ ์™€์ด์–ด, ๋ฒ„์ŠคํŠธ ์ œ์–ดํŒ(Burst control plate) ๋“ฑ๊ณผ ์ฐจ๋ณ„์ ์„ ๊ฐ–๋Š”๋‹ค. ์ฆ‰, ์ŠคํŠธ๋ฆฝ์€ ์ƒ๋Œ€์ ์œผ๋กœ ๋งค์šฐ ์ž‘์€ ๋†’์ด (๊ฒฝ๊ณ„์ธต ๋†’์ด๋ณด๋‹ค ์ž‘์€)๋ฅผ ๊ฐ€์ง๊ณผ ๋™์‹œ์— ์ „์ฒด ์ตํ˜• ํ‘œ๋ฉด์— ์„ค์น˜๋จ์œผ๋กœ์จ ํšจ๊ณผ์ ์ธ ์‹ค์† ์ œ์–ด ํšจ๊ณผ๋ฅผ ๊ฐ€์ง์—๋„ ์‹ค์† ์ด์ „์˜ ๋‚ฎ์€ ๋ฐ›์Œ๊ฐ์—์„œ์˜ ๊ณต๋ ฅ ์„ฑ๋Šฅ ์— ํฌ๊ฒŒ ์˜ํ–ฅ์„ ์ฃผ์ง€ ์•Š๊ฒŒ ๋œ๋‹ค. ์ข…๋ฐฉํ–ฅ ์ŠคํŠธ๋ฆฝ์˜ ์‹ค์ œ ์ ์šฉ ๊ฐ€๋Šฅ์„ฑ์„ ํ™•์ธํ•˜๊ธฐ ์œ„ํ•ด ์ŠคํŠธ๋ฆฝ์„ ์ˆ˜์ง์ถ• ํ’๋ ฅ ๋ฐœ์ „๊ธฐ(VAWT) ๋ชจ๋ธ์— ์ ์šฉํ•˜์—ฌ ์‹คํ—˜์ ์œผ๋กœ ๋ฐœ์ „ ์„ฑ๋Šฅ์˜ ํ–ฅ์ƒ์„ ํ™•์ธํ•˜์˜€๋‹ค. ์ด ๋•Œ, ์ˆ˜์ง์ถ• ํ’๋ ฅ ๋ฐœ์ „๊ธฐ์—์„œ ์ตํ˜•์€ ์ฃผ๊ธฐ์ ์ธ ๋ฐ›์Œ๊ฐ์˜ ๋ณ€๋™์„ ๊ฒช๊ธฐ์— ์ผ๋ฐ˜์ ์œผ๋กœ ๋Œ€์นญ ์ตํ˜•์„ ์‚ฌ์šฉํ•˜๊ฒŒ ๋œ๋‹ค. NACA0018 ์ตํ˜•์ด ๋„๋ฆฌ ์“ฐ์ด๋ฉฐ, ์ด์—๋”ฐ๋ผ ์‹ค์ œ ์ˆ˜์ง์ถ• ํ’๋ ฅ ๋ฐœ์ „๊ธฐ์— ์ŠคํŠธ๋ฆฝ์„ ์ ์šฉํ•˜๊ธฐ ์ „์— NACA0018 ์ตํ˜•์— ์ŠคํŠธ๋ฆฝ์„ ์ ์šฉํ•˜์—ฌ ์–‘๋ ฅ ๋ฐ ํ•ญ๋ ฅ์„ ์ธก์ •ํ•จ์œผ๋กœ์จ ์‹ค์† ์ œ์–ด ํšจ๊ณผ๋ฅผ ์กฐ์‚ฌํ•˜์˜€๋‹ค. SD7003์—์„œ์™€ ๋™์ผํ•˜๊ฒŒ ๊ธ‰๊ฒฉํ•œ ์‹ค์† ํ˜„์ƒ์ด ์ŠคํŠธ๋ฆฝ์— ์˜ํ•ด ์‚ฌ๋ผ์ง€๋ฉฐ ๊ทธ ๊ฒฐ๊ณผ ์‹ค์† ์ดํ›„์˜ ๋†’์€ ๋ฐ›์Œ๊ฐ์—์„œ ๋งค์šฐ ํ–ฅ์ƒ๋œ ์–‘ํ•ญ๋น„๋ฅผ ๊ฐ€์ง์„ ํ™•์ธํ•˜์˜€๋‹ค. VAWT ๋ชจ๋ธ์— ์ŠคํŠธ๋ฆฝ์„ ์ ์šฉํ•˜์—ฌ ๋ฐœ์ „ ์„ฑ๋Šฅ์„ ์ธก์ •ํ•œ ๊ฒฐ๊ณผ, ์ŠคํŠธ๋ฆฝ์— ์˜ํ•ด ์„ฑ๋Šฅ ๊ณ„์ˆ˜๊ฐ€ ์ƒ์Šนํ•จ์„ ํ™•์ธํ•˜์˜€์œผ๋ฉฐ, ์ด๋Š” ์ŠคํŠธ๋ฆฝ์˜ ์‹ค์† ์ œ์–ด ์žฅ์น˜๋กœ์„œ์˜ ์‹ค์ œ์  ๊ฐ€๋Šฅ์„ฑ์„ ๋ณด์—ฌ์ค€๋‹ค ํ•  ์ˆ˜ ์žˆ๋‹ค.We suggest longitudinal strips attached to an airfoil surface as a new stall control device. Their effects on the stall delay and flow modifications are experimentally investigated. The airfoil considered is SD7003 and the Reynolds numbers are Re = 60,000 and 180,000 based on the chord length and freestream velocity. The drag and lift forces on the airfoil are measured by varying the angle of attack from ฮฑ = 0ยฐ to 16ยฐ with and without strips. The optimal strip configuration is determined using a response surface method. Without strip, an abrupt stall occurs at ฮฑ = 11ยฐ and 13ยฐ for Re = 60,000 and 180,000, respectively, whereas the abrupt stall disappears with optimal strips. The lift and drag coefficients are significantly increased and decreased by the strips, respectively, at post-stall angles of attack. A corner vortex is generated at each corner of strip near the leading edge. Clockwise and counter-clockwise streamwise vortices are generated at the left- and right-facing corners, respectively, and they slowly move away from the corners while travelling downstream. These vortices provide additional momentum to the airfoil suction surface, resulting in fully attached flow above the strips and reattachment of flow above grooved surface. The longitudinal strips presented here are different from other devices such as the vortex generator, trip wire and burst control plate used for the stall control of low Reynolds number airfoil, in that the strips are installed nearly on the whole airfoil surface but with their heights lower than the boundary layer thickness, and produce positive control effects at post-stall angles of attack but little affect the aerodynamic performance at pre-stall angles of attack. To examine the applicability of the strips, we installed the strips to the vertical axis wind turbine (VAWT) model. For VAWTs a symmetric airfoil is commonly used because of the periodic change of angle of attack (minus to plus). NACA0018 airfoil is widely used, then we investigate the stall control effect of the strips by directly measuring drag and lift forces. The abrupt stall is modified to a broad stall and the lift-to-drag ratio in a post-stall region is significantly enhanced with the strips. In a VAWT models, the strips also increasing the performance of the wind turbine model showing that the applicability of the strips as a stall control devices.1. Introduction 1.1 Low Reynolds number airfoils and the effect of the laminar separation bubble (LSB) 1.2 Separation control devices 1.3 Objectives 2. Experimental setup 2.1 Two-dimensional experimental setup for direct force measurements 2.2 Parameters for a strip and shape optimization using a response surface method 2.3 Surface-oil visualization 2.4 Digital particle image velocimetry 2.5 Surface pressure measurements 3. Results and discussion 3.1 Shape optimizations using a response surface method and aerodynamic performance enhancements 3.2 The mechanisms responsible for the stall control 3.3 Effect of the strip length 4. Summary 5. Introduction 5.1 Wind power generation methods 5.2 The aerodynamic characteristics of VAWT 5.3 Objectives 6. Experimental setup 6.1 Two-dimensional experiment setup for a direct force measurement 6.2 Shape parameters for a VAWT model and direct torque measurements 7. Results and discussion 7.1 The aerodynamic performance of NACA0018 airfoil with and without the strips 7.2 The performance of VAWT model with and without strips 8. Summary and concluding remarksDocto
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