• 제목/요약/키워드: Probe angle

검색결과 229건 처리시간 0.059초

HR-MAS NMR Technique for Metabolic Profiling of Powdery Ginseng

  • Yoon, Dahye;Jo, Ick-Hyun;Kim, Suhkmann
    • 한국자기공명학회논문지
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    • 제20권3호
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    • pp.82-86
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    • 2016
  • Ginseng is used as a medicinal ingredient. The quality control of species, age, origin and manufacturing process is important. The metabolome of ginseng about quality was studied in many reports. Almost studies carried out the extract of ginseng, however, the reproducibility cannot be obtained using extracted sample. In this study, powdery ginseng samples were analyzed using high resolution-magic angle spinning nuclear magnetic resonance (HR-MAS NMR)-based metabolomics except extraction step. Sample was measured three times using 600 MHz NMR spectrometer equipped with nano probe. Reproducibility can be enhanced using this method and the metabolic profiles of ginseng were identified and quantified.

타원형 날개의 공력 특성 연구 (A Study on the Aerodynamic Load Characteristics of an Elliptic Airfoil)

  • 이기영;손명환;김해원
    • 한국군사과학기술학회지
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    • 제6권4호
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    • pp.29-37
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    • 2003
  • Using a wind tunnel testing, the aerodynamic load characteristics of an elliptic airfoil was described. The experimental data was obtained for angles of attack $-20^{\circ}$ to $+20^{\circ}$ with $2^{\circ}$ increments at a chord Reynolds number of $0.99{\times}105$ and $2.48{\times}105$. For each test case, chordwise suction pressure distributions and wake surveys were obtained. Static pressure measurements were made over a 10 sec averaging time at a 10 Hz sampling rate. For each case, wake survey was conducted with a pilot-static probe at 1.0c downstream from the trailing edge at very fine spacing to resolve the wake velocity deficit profile. As can be expected, suction pressure coefficient was increased with angle of attack. The normal force, CNmax, appeared peak value at the incidence angle of $12^{\circ}~14^{\circ}$, and the significant increase in profile drag at this range of angles of attack.

Features of the flow over a finite length square prism on a wall at various incidence angles

  • Sohankar, A.;Esfeh, M. Kazemi;Pourjafari, H.;Alam, Md. Mahbub;Wang, Longjun
    • Wind and Structures
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    • 제26권5호
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    • pp.317-329
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    • 2018
  • Wake characteristics of the flow over a finite square prism at different incidence angles were experimentally investigated using an open-loop wind tunnel. A finite square prism with a width D = 15 mm and a height H = 7D was vertically mounted on a horizontal flat plate. The Reynolds number was varied from $6.5{\times}10^3$ to $28.5{\times}10^3$ and the incidence angle ${\alpha}$ was changed from $0^{\circ}$ to $45^{\circ}$. The ratio of boundary layer thickness to the prism height was about ${\delta}/H=7%$. The time-averaged velocity, turbulence intensity and the vortex shedding frequency were obtained through a single-component hotwire probe. Power spectrum of the streamwise velocity fluctuations revealed that the tip and base vortices shed at the same frequency as that ofspanwise vortices. Furthermore, the results showed that the critical incidence angle corresponding to the maximum Strouhal number and minimum wake width occurs at ${\alpha}_{cr}=15^{\circ}$ which is equal to that reported for an infinite prism. There is a reduction in the size of the wake region along the height of the prism when moving away from the ground plane towards the free end.

레이저를 이용한 박판 버의 정밀측정 (Precision measuring of burrs on sheet metal using the laser)

  • 신홍규;홍남표;김헌영;김병희
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2003년도 춘계학술대회 논문집
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    • pp.1824-1827
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    • 2003
  • The sheet metal shearing process is normally used in the precision elements such as semi-conductor components. In precision elements, burrs usually reduce the quality of machined parts and cause interference, jamming and misalignment during assembly procedures and because of their sharpness, they can be safety hazard to personnel. Furthermore, not only burrs are hard to predict and avoid, but also deburring, the process of removing burrs, is time-consuming and costly. In order to get the burr-free parts, therefore, we developed the precise burr measuring system using the laser. The laser burr measuring system consists of the laser probe, the photo detector, the achromatic doublet lens, and the rotary & the X-Y table. In previous reports, we used simple vertical measuring method. But, as we used relatively bigger laser spot diameter and had the limited reflection angle, it was difficult to obtain the precise measuring results. So called, the spot size effect makes the profile of burr measured distorted and the burr height measured smaller. By introducing the novel laser measuring method which employing the achromatic lens system and the tilting mechanism, we could make the spot size smaller and get the appropriate beam direction angle. Through the experiments, the accuracy of the developed system is proved. The burr height measured during the punching process can be used for automatic deburring and in-situ aligning.

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드릴용 SRM의 최적운전을 위한 스위칭각 산정 (A Computing Switching Angle for Adaptive Operation of SRM for Drill)

  • 최경호;김남훈;백원식;김동희;노채균;김민회;황돈하
    • 대한전기학회논문지:전기기기및에너지변환시스템부문B
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    • 제50권11호
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    • pp.575-582
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    • 2001
  • This paper presents a calculating method of switching angle for adaptive switched reluctance motor (SRM) drive of a drill. The operation of the SRM is completely characterized by the flux linked by one phase winding which depends only on the current in that same phase winding and the rotor position. An efficiently adaptive SRM drive is possible on appropriately scheduling the commutation angles with accurate rotor position, supplied current value and speed information. An adaptive SRM drive with reduction torque ripple should be controlled by an optimized phase current control along with rotor position. Therefore, we are suggested a computing method of switching turn-on and off angles for adaptationally SRM operation with varied rotor speed and load. To probe the computing method, we have some simulation and experiment, it is shown a good result that can be computing the optimized switching angles for an electric drill motor.

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차량 원더링 계측을 위한 사선센서 적정 설치각도 결정 (Determining the Appropriate Installation Angle of Skewed Sensor to Measure Vehicle Wandering)

  • 오주삼;장경찬;김민성;장진환
    • 한국도로학회논문집
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    • 제10권3호
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    • pp.79-86
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    • 2008
  • 차량의 동적하중이 도로상에 작용하는 위치를 계측하기 위한 원더링 계측용 사선센서의 적정 설치각도를 제안하였다. 이를 위해서 테이프스위치 센서를 이용하여 원더링 계측용 장비를 개발하였고, 개발된 장비와 실험차량을 이용하여 평가용 자료를 수집하였다. 수집자료 분석 결과, 사선센서의 설치각도가 커질수록 원더링 수집자료의 오차가 감소하였고, 이러한 오차의 감소는 통계적으로도 의미가 있는 것으로 분석되었다. 그러나 사선센서를 $30^{\circ}$ 이상으로 설치할 경우, 탠덤축의 제원상의 이유로 인해 오류자료가 수집되는 것을 확인할 수 있었다. 따라서 본 연구에서는 국내 차량제원 등을 종합하여 원더링 계측용 사선센서의 적정 설치각도를 $20^{\circ}{\sim}25^{\circ}$로 제안하였다.

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초음파를 이용한 CFRP 복합재의 일방향 비파괴 평가 (One-Sided Nondestructive Evaluation of CFRP Composites By Using Ultrasonic Sound)

  • 임광희;장계림;최성록;예창희;류제성;임수환;한민규
    • 한국생산제조학회지
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    • 제20권1호
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    • pp.47-52
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    • 2011
  • It is well known that stiffness of composites depends on layup sequence of CFRP(carbon fiber reinforced plastics) laminates because the layup of composite laminates influences their properties. Ultrasonic NDE of composite laminates is often based on the backwall echoes of the sample. A pair of such transducers was mounted in a holder in a nose-to-nose fashion to be used as a scanning probe on composites. Miniature potted angle beam transducers were used (Rayleigh waves in steel) on solid laminates of composites. Experiments were performed to understand the behavior of the transducers and the nature of the waves generated in the composite (mode, wave speed, angle of refraction). C-scan images of flaws and impact damage were then produced by combining the pitch-catch probe with a portable manual scanner known as the Generic Scanner ("GenScan"). The pitch-catch signal was found to be more sensitive than normal incidence backwall echo of longitudinal wave to fiber orientation of the CFRP composites, including low level porosity, ply waviness, and cracks. Therefore, it is found that the experimentally Rayleigh wave variation of pitch-catch ultrasonic signal was consistent with numerical results and one-side ultrasonic measurement might be very useful to detect the defects.

옆미끄럼을 갖는 LEX/삼각 날개 형상에 대한 높은 받음각 와유동의 가시화 연구 (Visualization Study of High-Incidence Vortical Flow over the LEX/Delta Wing Configuration with Sideslip)

  • 손명환;이기영
    • 한국항공우주학회지
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    • 제30권5호
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    • pp.109-117
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    • 2002
  • 옆미끄럼이 있는 조건에서 LEX를 갖는 삼각날개의 와류 특성을 유동의 가시화에 의한 실험적 방법으로 연구하였다. 모델은 $65^{\circ}$ 후퇴각의 갖는 평판 날개이다. 자유 유동속도는 6.2 m/s이며, 이 속도와 날개뿌리 시위를 기준으로 한 레이놀즈 수는 $4.4\times10^5$ 이다. 받음각 범위와 옆미끄림각 범위는 각각 $16^{\circ}\sim28^{\circ}$$0^{\circ}\sim-15^{\circ}$ 이다. 미세수적과 레이저 평면광에 의한 가시화는 오공 프로브에 의한 측정으로부터 얻을 수 없었던 보다 자세한 와유동 구조를 관찰 할 수 있도록 하였다. 옆미끄럼각이 있는 경우, 바람쪽은 LEX 와류와 날개 와류의 상호작용과 붕괴가 촉진되는 반면, 바람반대쪽은 두 와류의 상호작용과 붕괴가 억제되었다.

양상태 소나에서의 자세각과 양상태각에 따른 표적 식별 정확도 비교 (Comparison of target classification accuracy according to the aspect angle and the bistatic angle in bistatic sonar)

  • 추연성;변성훈;추영민;최기융
    • 한국음향학회지
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    • 제40권4호
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    • pp.330-336
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    • 2021
  • 양상태 능동 소나에서 수중 표적의 산란 강도는 사용된 신호의 주파수, 표적과 음원사이의 각도를 의미하는 자세각, 표적과 수신기 사이의 각도를 나타내는 양상태각 등의 운용 변수에 따라 다르게 나타난다. 따라서 양상태 소나의 표적 탐지 및 식별 성능은 소나 운용 과정에서 표적, 음원, 그리고 수신기의 위치를 어떻게 변화시키느냐에 따라 그 성능이 달라질 수 있다. 본 연구에서는 양상태 소나 운용 시 자세각을 변화시키는 경우와 양상태각을 변화시키는 경우의 표적 식별 성능을 비교하여 어떤 변수를 변화시키는 것이 유리한지 평가하였다. 속이 비어있는 구와 실린더를 식별하는 시나리오를 가정하였으며, 유한요소법 기반의 음향 산란 시뮬레이션을 이용하여, 서포트 벡터 머신으로 두 표적을 분류하고 정확도를 비교하는 방법으로 성능을 비교하였다. 표적의 산란 신호만을 고려하기 위하여, 해저면 잔향의 효과는 고려하지 않았다. 비교 결과, 자세각을 고정한 상태에서 주파수와 양상태각으로 정의되는 산란 강도를 이용하는 것이 우수한 평균 분류 정확도를 보여주었으며, 이는 양상태 소나를 이용하여 구와 실린더를 식별하고자 하는 경우, 음원의 위치를 고정시킨 상태에서 수신기를 이동하여 양상태각을 변화시키는 것이 표적 식별에 더 효과적임을 보여준다.

연장된 앞전을 갖는 델타형 날개에서의 와류 상호작용에 관한 연구 (Investigation of Vortex Interactions over a Delta Wing with the Leading Edge Extension)

  • 이기영;손명환;장영일
    • 한국군사과학기술학회지
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    • 제4권2호
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    • pp.215-224
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    • 2001
  • An experimental investigation was conducted on the interaction of vortices over a delta wing with the leading edge extension for three angles of attack($16^{\circ},\; 24^{\circ} \;and\; 28^{\circ}$) at Reynolds number of $1.76{\times}10^6.$ The experimental data included total pressure contours and velocity vectors using 5-hole probe measurements. Constant total pressure coefficient contours show the LEX vortex moves downward and outboard, while the wing vortex exhibited an inboard and upward migration. At near the trailing edge, these vortices reveal a direct interaction between the wing and LEX vortex, featuring a coiling of vortex cores about each other. The combined effect of the interaction of these two vortices and proximity to the wing surface results in the increase of the suction peak. This is in contrast to the result obtained on the delta wing alone configuration, where the effect of the vortex breakdown was manifested. The interaction of the wing and LEX vortices is more pronounced at higher AOA.

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