• 대한기계학회논문집B
• /
• 제20권8호
• /
• pp.2561-2571
• /
• 1996

The flow in the turbomachinery is very unsteady due to the stator-rotor interaction. It has been indicated that the stator-rotor interaction has three distinct causes of unsteadiness: that is, the viscous vortex shedding, wake rotor interaction and potential stator-rotor interaction. In this paper, the mechanism of unsteady potential interaction and wake interaction in the stator-rotor stage flow is numerically investigated in two-dimensional view point. The numerical technique used is the upwind scheme of Van Leer's Flux Vector Splitting(FVS) and cubic spline interpolation is applied on zonal interface. Then, the flow field of a compressor stage composed of NACA 65410 is analyzed. Flow fields are found to be simulated reasonably by this method and the sensitivity due to back-pressure variation is more stronger than rotor-velocity variation.

• 전자공학회논문지
• /
• 제50권5호
• /
• pp.102-111
• /
• 2013

본 연구에서는 4K UHD($3840{\times}2160$) 영상을 실시간 복호화하기 위한 $4{\times}4$ 블록 병렬 보간 H.264/AVC 움직임보상기를 제안한다. 연산처리 성능을 향상시키기 위해 보간 연산을 $4{\times}4$ 블록 단위로 병렬화시켰으며, 병렬 보간 연산에서 필요한 메모리 대역폭을 확장하기 위해 $9{\times}9$개의 메모리 어레이를 가진 2D 캐쉬 버퍼 구조를 설계하였다. 그리고 2D 캐쉬 버퍼는 검색영역 간 재사용 기법을 적용하여 참조화소의 중복저장을 최소화하였으며, $4{\times}4$ 블록 병렬 보간 필터는 3단(수평 수직 1/2부화소, 대각선 1/2부화소, 1/4부화소) 평면 보간 연산 파이프라인 구조로 설계하여 연산회로를 고속화시켰다. 0.13um 공정에서 시뮬레이션한 결과, 161K게이트의 H.264/AVC 움직임보상기는 동작주파수 150MHz에서 4K UHD급 동영상을 초당 72프레임으로 실시간 처리하는 성능을 보였다.

• 전자공학회논문지
• /
• 제50권6호
• /
• pp.145-155
• /
• 2013

본 연구에서는 8K UHD($7680{\times}4320$) 영상을 실시간 부호화하기 위한 $4{\times}4$ 블록 부화소 움직임추정기를 제안한다. 연산처리성능을 향상시키기 위해 보간 연산을 $4{\times}4$ 블록 단위로 병렬화시켰으며, 병렬 보간 연산에서 필요한 메모리 대역폭을 확장하기 위해 $10{\times}10$개의 메모리 어레이를 가진 2D 캐쉬 버퍼 구조를 설계하였다. 그리고 2D 캐쉬 버퍼는 검색영역 간 재사용 기법을 적용하여 참조화소의 중복저장을 최소화하였으며, $4{\times}4$ 블록 병렬 보간 필터는 3단(수평 수직 1/2부화소, 대각선 1/2부화소, 1/4부화소) 평면 보간 연산 파이프라인 구조로 설계하여 연산회로를 고속화시켰다. 0.13um 공정에서 시뮬레이션한 결과, 436.5K게이트의 $4{\times}4$ 블록 부화소 움직임추정기는 동작주파수 187MHz에서 8K UHD급 동영상을 초당 30프레임으로 실시간 처리하는 성능을 보였다.

• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 1999년도 유체기계 연구개발 발표회 논문집
• /
• pp.163-169
• /
• 1999

The numerical procedure has been developed for simulating incompressible viscous flow around a turbine stage with rotor-stator interaction. This study solves 2-D unsteady incompressible Navier-Stokes equations on a non-orthogonal curvilinear coordinate system. The Marker-and-Cell concept is applied to efficiently solve continuity equation. To impose an accurate boundary condition, O-H multiblocked grid system is generated. O-type grid and H-type grid is generated near and outer rotor-stator The cubic-spline interpolation is applied to handle a relative motion of a rotor to the stator. Turbulent flows have been modeled by the Baldwin- Lomax turbulent model. To validate present procedure, the time averaged pressure coefficients around the rotor and stator are compared with experiment and a good agreement obtained.

• 센서학회지
• /
• 제28권4호
• /
• pp.240-245
• /
• 2019

Phase interpolation is widely adopted in frequency synthesizers and clock-and-data recovery systems to produce an intermediate phase from two existing phases. The intermediate phase is typically generated by combining two input phases with different weights. Unfortunately, this results in non-uniform phase steps. Alternatively, the intermediate phase can be generated by successive approximation, where the interpolated phase at each approximation stage is obtained using the same weight for the two intermediate phases. As a proof of concept, this study presents a 2-GHz 8-bit successive approximation digital-to-phase converter that is designed using 65-nm CMOS technology. The converter receives an 8-phase clock signal as input, and the most significant bit (MSB) section selects four phases to create two sinusoidal waveforms using a harmonic rejection filter. The remaining least significant bit (LSB) section applies the successive approximation to generate the required intermediate phase. Monte-Carlo simulations show that the proposed converter exhibits 0.46-LSB integral nonlinearity and 0.31-LSB differential nonlinearity with a power consumption of 3.12 mW from a 1.2-V supply voltage.

• Journal of Biosystems Engineering
• /
• 제42권2호
• /
• pp.117-125
• /
• 2017

Purpose: Damage to pulse crops by wild birds is a serious problem. The damage is to such an extent that the rate of damage during the period between seeding and cotyledon stages reaches 54.6% on an average. In this study, a crop-position detection method was developed wherein infrared (IR) sensors were used to determine the cotyledon position under a vinyl mulch. Methods: IR sensors that helped measure the temperature were used to locate the cotyledons below the vinyl mulch. A single IR sensor module was installed at three locations of the crops (peanut, red lettuce, and crown daisy) in the cotyledon stage. The representative thermal response of a $16{\times}4$ pixel area was detected using this sensor in the case where the distance from the target was 25 cm. A spatial image was applied to the two-dimensional temperature distribution using a non-integral moving-average method. The collected data were first processed by taking the moving average via interpolation to determine the frame where the variance was the lowest for a resolution unit of 1.02 cm. Results: The temperature distribution was plotted corresponding to a distance of 10 cm between the crops. A clear leaf pattern of the crop was visually confirmed. However, the temperature distribution after the normalization was unclear. The image conversion and frequency-conversion graphs were obtained based on the moving average by averaging the points corresponding to a frequency of 40 Hz for 8 pixels. The most optimized resolutions at locations 1, 2, and 3 were found on 3.4, 4.1, and 5.6 Pixels, respectively. Conclusions: In this study, to solve the problem of damage caused by birds to crops in the cotyledon stage after seeding, the vinyl mulch is punched after seeding. The crops in the cotyledon stage could be accurately located using the proposed method. By conducting the experiments using the single IR sensor and a sliding mechanical device with the help of a non-integral interpolation method, the crops in the cotyledon stage could be precisely located.

• 한국전산유체공학회지
• /
• 제5권2호
• /
• pp.38-46
• /
• 2000

It has been indicated that the rotor/stator interaction has distinct causes of unsteadiness, such as the viscous vortex shedding, wake/stator interaction and potential rotor/stator interaction. In this paper, the mechanism of unsteady potential interaction in one stage axial compressor is numerically investigated for blade row ratio 1:1 and 2:3 at design point and for blade row ratio 2:3 at off-design point in two-dimensional view point. The numerical technique used is the upwind scheme of Van-Leer's Flux Vector Splitting(FVS) and Cubic spline interpolation is applied on zonal interface. In this study the flow unsteadiness due to potential interaction are found to be larger in blade row ratio 2:3 than in 1:1. The total pressure rise in blade row ratio 2:3 is closer to the real value in design point than that in 1:1. The change of unsteady pressure amplitude according to the variation of stator exit pressure is very small.

• JSTS:Journal of Semiconductor Technology and Science
• /
• 제15권6호
• /
• pp.695-702
• /
• 2015

A 1-V 1.6-GS/s 5.58-ENOB flash ADC with a high-speed time-domain comparator is proposed. The proposed time-domain comparator, which consumes low power, improves the comparison capability in high-speed operations and results in the removal of preamplifiers from the first-stage of the flash ADC. The time interpolation with two factors, implemented using the proposed time-domain comparator array and SR latch array, reduces the area and power consumption. The proposed flash ADC has been implemented using a 65-nm 1-poly 8-metal CMOS process with a 1-V supply voltage. The measured DNL and INL are 0.28 and 0.41 LSB, respectively. The SNDR is measured to be 35.37 dB at the Nyquist frequency. The FoM and chip area of the flash ADC are 0.38 pJ/c-s and $620{\times}340{\mu}m^2$, respectively.

• 대한기계학회논문집B
• /
• 제25권11호
• /
• pp.1518-1526
• /
• 2001

In this paper, the mechanism of unsteady potential interaction and wake interaction in one stage axial turbine is numerically investigated at design point in two-dimensional viewpoint. The numerical technique used is the upwind scheme of Van-Leer's Flux Vector Splitting (FVS) and Cubic spline interpolation is applied on zonal interface between stator and rotor. The inviscid analysis is used to embody the influence of potential interaction only and viscous analysis is used to embody the influences of both potential interaction and wake interaction at the same time. The potential-flow disturbance from the stator into a rotor passage and the periodic blockage effect of rotor produce the unsteady pressure on the blade surface in inviscid analysis. After the wake is cut by rotor, two counterrotating votical patterns flanking the wake centerline in the passage are generated. So, these phenomena magnify the unsteady pressure in viscous analysis than that in inviscid analysis. The resulting unsteady forces on the rotor, generated by the combined interaction of the two effects by potential and wake interaction, are discussed.

• 대한토목학회논문집
• /
• 제38권6호
• /
• pp.831-838
• /
• 2018

본 논문에서는 합류부 배수영향을 받는 지점에서 유량을 산정할 수 있는 방법을 제안하였다. 먼저, 최근 2개의 홍수사상에 대한 HEC-RAS 부정류 모의를 수행하여 모형을 보정하였으며, 관심구간 상하류 수위와 유량과의 관계 그래프를 작성하고 크리깅 보간을 수행함으로써 HPG (Hydraulic Performance Graph)를 작성하였다. 대상 홍수기간 동안 HPG와 상하류 연속 수위 자료를 이용하여 구간 유량을 산정하였고, ADVM 같은 자동유량측정 자료와 비교하여 비교적 잘 일치하는 것을 확인하였다. 본 연구결과는 수위-유량 관계곡선의 이력현상이 큰 배수영향 구간에서 유량을 산정하는데 경제적이고 실용적인 방법을 제공할 것이다.