• 대한기계학회논문집
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• 제18권4호
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• pp.977-985
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• 1994

New computer-aided calibration methods for the hot-wire and split film probes are presented. The proposed modified king's law takes into account instantaneous flow angle as well as the variation of calibration coefficients due to the total velocity magnitude change. It is found that the look-up table method has many advantages with respect to the accuracy on data and reducing run time for calibration over other conventional methods. In order to investigate the local sensitivity of the static calibration, a dynamic calibration procedure is also carried out.

• 대한전자공학회논문지TC
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• 제37권5호
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• pp.17-24
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• 2000

자체 설계 및 제작된 개방단말 동축선 프로브를 이용하여 마른 모래의 복소 유전율을 측정하였다. 프로브의 간단한 교정 방안으로 순수한 물에 대해 측정된 반사계수와 수치계산한 반사계수간의 위상차를 모래에 대해 측정된 반사계수의 위상에 뺐다. 그 다음 마른 모래에 대해 측정된 반사계수를 개선된 가상의 동축선 모델에 대입하여 복소 유전율을 환산하였다. 동일한 마른 모래에 대해 측정된 정확한 측정자료와 비교함으로써 본 측정방법의 정확성을 입증하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제20권2호
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• pp.116-116
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• 1996

This paper is concerned with a method for calibrating five-hole probes of both angle-tube and prismatic geometries to measure local total and static pressures and the magnitude and direction of the mean velocity vector. Descriptions of the calibration technique, the typical calibration data, and an accompanying discussion of the interpolation procedure are included. The flow properties are determined explicitly from measured probe pressures using calibration data. Flow angles are obtained within the deviation angle of 1.0 degree and dynamic pressures within 0.03 with 95% certainty. The variations in the calibration data due to Reynolds number are also discussed. For the range of Reynolds number employed, no effect was detected on the pitch, yaw and total pressure coefficients. However, the static pressure coefficient showed change to cause minor variations in the magnitude of the calculated velocity vector. To account for these variations, average correction factors need to be incorporated into the static pressure coefficient.

• Journal of Advanced Marine Engineering and Technology
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• 제20권2호
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• pp.48-56
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• 1996

This paper is concerned with a method for calibrating five-hole probes of both angle-tube and prismatic geometries to measure local total and static pressures and the magnitude and direction of the mean velocity vector. Descriptions of the calibration technique, the typical calibration data, and an accompanying discussion of the interpolation procedure are included. The flow properties are determined explicitly from measured probe pressures using calibration data. Flow angles are obtained within the deviation angle of 1.0 degree and dynamic pressures within 0.03 with 95% certainty. The variations in the calibration data due to Reynolds number are also discussed. For the range of Reynolds number employed, no effect was detected on the pitch, yaw abd total pressure coefficients. However, the static pressure coefficient showed change to cause minor variations in the magnitude of the calculated velocity vector. To account for these variations, average correction factors need to be incorporated into the static pressure coefficient.

• 대한기계학회논문집
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• 제18권9호
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• pp.2358-2367
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• 1994

This paper presents techniques for evaluation and compensation of total measuring errors in a commercial CMM. The probe errors as well as the machine geometric errors are assessed from probing of the mechanical artefacts such as shpere, step, and rings. For the error compensation, the integrated volumetric error equations are considered, including the probe error adn the machine geometric error. The error compensation is performed on the absolute scale coordinate system, in order to overcome the redundant degree of freedom in the CMM with multi-axis probe. A interface box and corresponding software driver are developed for data intercepting/correction between the machine controller and machine, thus the volumetric errors can be compensated in real time with minimum interference to the operating software and hardware of a commercial CMM. The developed system applied to a practical CMM installed on the shop floor, and demonstrated its performance.

• 동력기계공학회지
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• 제10권4호
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• pp.56-64
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• 2006

This paper shows the development process of a straight-type five-hole pressure probe for measuring three-dimensional flow velocity components. The data reduction method using a bi-cubic curve-fitting program in a new calibration map was introduced in this study. This new calibration map can be applied up to the application angle, ${\pm}55^{\circ}$ of a probe. As a result, for the application angle of ${\pm}45^{\circ}$, an error for yaw and pitch angles appeared from $-1.76^{\circ}\;to\;1.83^{\circ}$ and from $-1.91^{\circ}\;to\;1.75^{\circ}$, respectively. Moreover, an error for a vector magnitude and a static pressure compared with a dynamic one showed from -7.83% to 4.87% and from -0.73 to 0.77, respectively. Even though this data reduction method showed unsatisfactory errors in a vector magnitude, it resulted in an easy and simple application method. Especially, when it was applied to an actual flow field including a swirling flow, a good result came out on the whole. However, in order to obtain a better result, it is thought that a more sophisticated interpolation method needs to be introduced.

• 동력기계공학회지
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• 제14권1호
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• pp.40-46
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• 2010

This paper shows the development process for measuring three-dimensional flow velocity components in a web-browser. The system is developed in an embeddable C/C++ interpreter Ch and Ch-CGI toolkit. The interface for the web-based measurement system consists of a set of web HTML files and Ch files for CGI. All of data in web browser are passed to Ch-CGI script to generate the output of new HTML file. PC-Server and PC-Client can submit measurement parameters and receive the text/graphical results each other. PC-Client can control the test equipment by using a parameters that received from PC-Server. It also can pass the test results between the web-based measurement system. In summary, the designed measurement system is evaluated, the outputs shown well on the web browser.

• 대한전자공학회논문지SD
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• 제49권6호
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• pp.25-34
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• 2012

본 논문에서는 near-field scanning (NFS) 시스템을 위한 새로운 보정 방법을 제시하였다. 제안된 교정 방법은 새로운 near-field probe (NFP)와 circular patch patterns (CPPs) and meander patterns (MPs) 같은 새로 고안된 패턴으로 구성되어 있다. 제안된 패턴들은 IEC61967-2과 6에 언급된 기존의 방법과 비교해 공간 해상도을 개선하고 NFP의 교정 절차를 단순화하기 위해 사용하였다. 또한 감쇄 특성에 대한 NFP의 길이 효과를 8mm와 30mm의 길이를 가지고 조사하였다. 이러한 특성을 위해 지름 (D)가 20, 40, 60, 그리고 100mm의 CPP를 만들었고 여러 가지 폭과 간격을 가지는 MP를 설계하고 제작하였다. 단순화된 교정 절차를 이용하여 공간 해상도와 측정 높이 사이의 역 관계를 발견하였다. 테스팅 결과는 측정 높이 $200{\mu}m$에서 $120{\mu}m$의 공간해상도를 복잡한 수정 알고리듬 없이 8GHz 아래에서 얻을 수 있음을 보였다. 제작 단가를 위해 모든 패턴과 NFP는 일반적인 고가의 LTCC 대신 저가의 PCB (FR-4)을 이용해 실현하였다. 이결과를 칩 수주 EMC 사용 가능성을 검증하기 Sub-micron scale 동작이 가능한 NFSS을 제작하였고, 제안된 NFP를 이용하여 사용 칩의 측정결과 $200{\mu}m$ 패턴의 형태를 정확하게 묘사가 가능한 수준의 해상도를 확보하여 칩 수준 EMC 검증에 사용 할 수 있음을 증명하였다.

• 한국항공우주학회지
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• 제47권12호
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• pp.831-840
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• 2019

플러시 대기자료 측정장치는 비행체 표면에서 측정되는 압력 데이터를 이용하여 대기자료를 예측한다. FADS는 돌출된 프로브가 없으므로 고성능 항공기, 스텔스 비행체 및 극초음속 비행체에 적합하다. 본 논문에서는 구-원추 형상을 갖는 비행체에 대해서 아음속부터 초음속 비행까지 대기자료를 예측할 수 있는 FADS의 교정 절차와 계산 알고리즘을 제시한다. 표면 압력 데이터 측정을 위해 노즈부 표면에 5개 플러시 압력공들을 마련하였다. 유동각 예측과 압력 관련 변수의 예측을 분리하는 개념이며, 아음속 유동의 포텐셜 유동해와 극초음속 유동의 수정 뉴톤식을 결합한 압력모델을 사용한다. 교정 압력 데이터는 Euler 방정식을 푸는 전산유체역학 코드를 만들어서 마흐수 0.5 ~ 3.0의 범위에서 구축하였다. 비행 마흐 수 0.6~3.0, 받음각과 옆미끄럼각은 각각 -10° ~ +10°의 범위에서 여러 비행조건에 대해서 테스트를 수행하였다. 예측된 대기자료는 받음각, 옆미끄럼각, 마흐수, 자유류 정압이며 참고 데이터와 비교하여 정확도를 분석하였다.