http://chineseinput.net/에서 pinyin(병음)방식으로 중국어를 변환할 수 있습니다.
변환된 중국어를 복사하여 사용하시면 됩니다.
YOLO 기반 개체 검출과 Node.js 서버를 이용한 반려견 행동 분류 시스템 구현
조용화,이혁재,김영훈,Jo, Yong-Hwa,Lee, Hyuek-Jae,Kim, Young-Hun 한국융합신호처리학회 2020 융합신호처리학회 논문지 (JISPS) Vol.21 No.1
본 논문은 실시간 영상 분석을 통해서 반려견에 대한 객체를 추출해 내고, 추출된 이미지로부터 반려견 행동을 분류하는 방법을 구현한다. 반려견 객체 탐지를 위해서 Darknet YOLO를 사용하였으며, 추출된 이미지로부터 행동 패턴 분류는 구글에서 제공하고 있는 Teachable Machine을 이용하였다. 학습된 Teachable Machine은 구글 드라이브에 저장되어 node.js 서버 상에서 ml5.js로 구현하여 사용할 수 있다. 분류된 행동 패턴 결과는 사용자의 스마트 폰 또는 PC로 실시간 전송되며, 언제 어디서든 확인 가능할 수 있게 node.js 서버에서 socket.io 모듈을 사용해서 상호반응 웹 서버를 구현하였다. This paper implements a method of extracting an object about a dog through real-time image analysis and classifying dog behaviors from the extracted images. The Darknet YOLO was used to detect dog objects, and the Teachable Machine provided by Google was used to classify behavior patterns from the extracted images. The trained Teachable Machine is saved in Google Drive and can be used by ml5.js implemented on a node.js server. By implementing an interactive web server using a socket.io module on the node.js server, the classified results are transmitted to the user's smart phone or PC in real time so that it can be checked anytime, anywhere.
반복된 제트 충돌을 갖는 내부 유로의 평균 열전달 계수 측정
박승덕,이기선,김석범,조용화,전창수,곽재수,허재성,Park, Seoung Duck,Lee, Ki Seon,Kim, Sug Bum,Jo, Yong Hwa,Jeon, Chang Soo,Kwak, Jea Su,Huh, Jae-Sung 항공우주시스템공학회 2008 항공우주시스템공학회지 Vol.2 No.4
Averaged heat transfer coefficients were measured in a turbine blade internal cooling passage model with three blockage walls. Each blockage wall was equipped with 9 staggered holes or slots in order to create different shaper of repeated jet impingement. The effect of jet shape on the averaged heat transfer coefficient was studied by the copper-thermocouple method and three Reynolds number of 10,000, 20,000, and 30,000 were tested. Results showed that the repeated stagger jets could increase the averaged heat transfer coefficient by at least 9 times compared to the smooth channel cases. Due to the large pressure drop induced by the repeated jet impingement, the thermal performance was less than 1 for all cases and decreased as the Reynolds number increased. Among the tested cases, the widest slot showed the best thermal performance. The measurement results showed that the thermal performance of the heat transfer augmentation by repeated stagger jets could be improved by altering the jet shape, and other shape of impingement jet will be studied in near future.
블레이드 팁의 Groove 형상이 터빈 캐스케이드 팁 열전달 계수분포에 미치는 영향에 대한 실험적 연구
노영철(Young Cheol Nho),조용화(Yong Hwa Jo),이용진(Youn Jin Lee),김학봉(Hark-Bong Kim),곽재수(Jae Su Kwak) 한국추진공학회 2010 한국추진공학회 학술대회논문집 Vol.2010 No.5
본 연구에서는 팁 형상이 가스터빈 블레이드의 팁 열전달에 미치는 영향을 알아보기 위하여 선형 캐스케이드의 블레이드에 설치된 평면 팁, 스퀼러 팁, Groove 팁들에 대하여 열전달 계수가 측정되었다. 블레이드 팁에서의 열전달 계수는 색상검출방식에 기반을 둔 천이액정법을 이용하여 측정되었으며 각각의 팁 형상에 대하여 팁 간극은 블레이드 스팬의 1.5%와 2.3%로 변경 하에 실험을 수행하였다. 캐스케이드 출구 속도와 블레이드 코드길이에 기초를 둔 Reynolds 수는 2.48×10<SUP>5</SUP> 이다. Groove 팁 표면에서의 열전달 계수는 평면 팁보다 낮게 측정되었으며, 특히 흡입면을 따라 경사진 홈이 파인 팁에서는 스퀼러 팁보다 낮은 열전달 계수가 측정되었다. In this study, the conventional plane tip, double squealer tip, and various groove tip blades were tested in a linear cascade in order to measure the effect of the tip shapes on tip surface heat transfer coefficient distributions. Detailed heat transfer coefficient distributions were measured using a hue-detection based transient liquid crystals technique. Two tip gap clearances of 1.5% and 2.3% of blade span were investigated and the Reynolds number based on cascade exit velocity and chord length was 2.48×10<SUP>5</SUP>. Results showed that the overall heat transfer coefficients on the tip surface with various grooved tips were lower than those with plane tip blade. The overall heat transfer coefficient on grooved along suction side tip was lower than that on the squealer tip.
안최란,기효진,진병규,김정균,김석범,조용화,노영철,최용덕,곽재수,최용규,An, Choiran,Ki, Hyojin,Jin, Byeong Kyou,Kim, Jung Kyun,Kim, Sug Bum,Jo, Yong Hwa,Nho, Young Cheol,Choi, Yong Duk,Kwak, Jae Su,Choi, Yong Gyu 항공우주시스템공학회 2008 항공우주시스템공학회지 Vol.2 No.3
We have fabricated pressure sensitive paint films consisting of PtTFPP activators dispersed in fluorinated polymer matrix. This matrix material is unique in its composition and structure. We evaluated the oxygen quenching effects, and thus the pressure sensitivity, of the fabricated films in terms of various processing parameters. Based on the experimental results, we anticipate that a good but new pressure sensitive paint would be presented through further elaboration of the polymer compositions and optimization of the processing conditions.