• 한국ITS학회 논문지
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• 제18권6호
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• pp.233-240
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• 2019

본 논문에서는 최근 5G 통신기술의 발전으로 인해 LTE와 5G 대역을 모두 커버할 수 있는 안테나가 필요로 하고 있으며, 각 대역에서 공진 주파수 대비 10%이상의 대역폭을 만족하기 위해 통합공공망(LTE)과 5G 주파수 이중대역 커버용 단일 급전 안테나를 설계, 제작하였다. 기본형 다이폴 안테나의 방사소자를 평면형 구조를 채택하였으며, 설계된 안테나는 700 MHz 안테나의 경우 동축케이블 급전 및 balun을 형성시켜 설계되었으며, 3.5GHz의 경우는 700 MHz 방사소자 급전부로부터 각각 수직 연장 후 'ㄷ'자 모양으로 접은 형태로 balun이 필요 없고 700 MHz 대역의 방사소자가 3.5 GHz 대역 방사소자의 반사판 역할을 하도록 설계하였다. 이로써, 700MHz 대역 -10 dB 대역폭 104 MHz(14.8%)과 3.5GHz 대역 -10 dB 대역폭 660 MHz(18.8%)을 나타내었고, 방사패턴 특성으로 700 MHz대역에서는 이득 8.46 dBi, 빔폭 E-plane 55°, H-plane 81°와 3.5 GHz 대역에서는 이득 6.14 dBi, 빔폭 E-plane 79°, H-plane 49°를 각각 얻었다.

• Bulletin of the Korean Chemical Society
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• 제8권3호
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• pp.147-149
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• 1987

The out-of-plane bending, vibrational-rotational FT-IR spectra of dichloroborane molecule were analyzed. The band centers are 785.992, 785.723, 647.217, and 646.997 $cm^{-1}$ and centrifugal distortion constants are $2.2{\times}10^{-6},\;5.5{\times}10^{-6},\;0.2{\times}10^{-6}$, and $0.7{\times}10^{-6}cm^{-1}$ for $H^{11}B^{35}Cl_2$, $H^{11}B^{35}Cl^{37}Cl$, $D^{11}B^{35}Cl_2$, and $D^{11}B^{35}Cl^{37}Cl$, respectively. The theoretical spectrum of $D^{11}B^{36}Cl_2$ was plotted to conform the molecular constants and the rotational constants for the first excited vibrational state of this molecule were A' = 1.165932, B' = 0.106166, and C' = 0.097229 $cm^{-1}$. The calculated spectra were in good agreement with the observed spectra.

• 한국ITS학회 논문지
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• 제11권1호
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• pp.42-52
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• 2012

본 논문에서는 UWB (Ultra Wide Band) high 대역 (중심 주파수 : 9.5 GHz, -10 dB 대역폭 : 600 MHz, 6.4 %)의 차량 측후방 레이더 센서용 도파관 안테나를 설계 및 제작하였다. 안테나는 대역폭이 넓고 구조가 간단한 프로브 급전 구형도파관을 이용하였다. 본 연구의 차량 레이더 시스템에 있어서 송수신 안테나의 큰 격리도 특성을 얻는 것이 설계의 중요한 변수이다. 따라서 두 도파관 안테나를 E-면과 H-면 배열하였을 시 격리도 특성을 시뮬레이션 하였다. 그 결과 도파관 안테나의 $TE_{10}$ 모드에 의하여 E-면 배열 보다 H-면 배열의 격리도 특성이 우수한 것을 확인하였다. 따라서 H-면 배열된 송수신 도파관 안테나를 T-형 레이더 모듈에 장착하여 안테나의 특성을 검출하였다. T-형 모듈에 장착된 송수신 안테나의 -10 dB 대역폭은 각각 1000 MHz (10.52 %)와 1090 MHz (11.47 %)로 측정되었고 격리도 (S21)는 요구 대역 내에서 -50 dB 이하로 측정되었다. 송수신 안테나의 최대이득은 각각 7.65 dBi와 7.26 dBi로 나타났으며 H-면 빔폭은 $64^{\circ}$, $65^{\circ}$로 측정되어 차량 측후방 레이더 센서용 안테나로 적합함을 확인하였다.

• Archives of Plastic Surgery
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• 제33권2호
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• pp.155-160
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• 2006

Although several reports have been introduced about dual plane augmentation mammaplasty, the description of periareolar approach dual plane augmentation mammaplasty was few. This article describes specific characteristics, and different classification and techniques for the periareolar dual plane breast augmentation while postoperative scars resulted from inframammary crease approach caused complaints. A total of 124 patients(248 breasts) had periareolar dual plane augmentation surgery from 1998 to 2004. Anatomic implants were used in 43 cases. Most of the patients were satisfied with the outcomes of periareolar dual plane augmentation. Periareolar dual plane augmentation mammaplasty adjusts implant and tissue relationships to ensure adequate soft-tissue coverage while optimizing implant-breast parenchymal dynamics to offer increased benefits and fewer faults compared to a single pocket location in a wide range of breast types with minimal scars. Two types of dual plane classifications are discussed in this study for the periareolar approach exclusively. The boundaries of retroglandular dissection remain constant, as the costal origin of pectoralis major are divided. Type A dual plane implies that the inferior edge of pectoralis muscle lies below the inferior areolar border, and type B dual plane implies that the inferior edge lies above the superior areolar border.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회B
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• pp.2567-2572
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• 2007

The suppression of fluid force acting on a square prism near plane wall was studied by attaching fences on the corners of the prism. The height of the fence was 10% of the square width and the range of Reynolds number considered was Re=$2.0{\times}10^4$. The experimental parameters were the attaching position and numbers of fences, the space ratios G/B(G/B=0.1${\sim}$1.2) between prism and plane wall. The average drag coefficients were increased and the average lift coefficients were decreased and increased with the space ratios toward plane wall. The drag of the prism was reduced average 7.6% with the space ratios by attaching the normal fence at the rear and upper corner and the horizontal normal fence at the rear and lower corner on the prism. In this case, the separated flow at the front and upper corner was reattached on the upper side of the prism and the vortex streets between the prism and plane wall were appeared more slowly than that of prism without fences.

• 대한기계학회논문집B
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• 제29권2호
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• pp.214-223
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• 2005

The characteristics of flow on two parallel plane jets was experimentally investigated. The two nozzles each with an aspect ratio of 20 were separated by 6 nozzle widths. Reynolds number based on nozzle width was set to 5,000 by nozzle exit velocity. The particle image velocimetry and pressure transducer were employed to measure turbulent velocity components and mean static pressure, respectively. In case of unventilated parallel plane jets, it was shown that a recirculation zone with sub-atmospheric static pressure was bounded by the inner shear layers of the individual jets and the nozzles plated. There was no recirculation zone in the ventilated parallel plane jets. It was found that the spanwise turbulent intensities of unventilated jets were higher than those of ventilated jets because of the interaction of jets, and the streamwise turbulent intensities of ventilated jets were higher than those of unventilated jets because of the effect of entrainment.

• 대한기계학회논문집B
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• 제27권6호
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• pp.766-772
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• 2003

The pseudospectral method for stability analysis was used to find the most influential disturbance mode for transition of plane channel flows and Blasius flow at their critical Reynolds numbers. A number of various oblique disturbance waves were investigated for their pseudospectra and resolvent norm contours in each flow, and an exhaustive search method was employed to find the disturbing waves to which the flows become most unstable. In plane Poiseuille flow an oblique disturbance with a wavelength of 3.59h (where h is the half channel width) at an angle $28.7^{\circ}$ was found to be the most influential for the flow transition to turbulence, and in plane Couette flow it is an oblique wave with a wavelength of 3.49h at an angle of $19.4^{\circ}$. But in Blasius flow it was found that the most influential mode is a normal wave with a wavelength of $3.44{\delta}_{999}$. These results imply that the most influential disturbance mode is closely related to the fundamental acoustic wave with a certain shear sheltering in the respective flow geometry.

• 대한기계학회논문집B
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• 제28권7호
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• pp.834-841
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• 2004

Experimental study on the three-dimensional topology of hairpin packet structures in turbulent boundary layers were carried out. Two different Reynolds number based on momentum thickness, Re$\sub$$\theta$/=514 and 934 were generated in a blowing type wind tunnel under the condition of zero pressure gradient. Simultaneous measurements of velocity fields at a wall-normal plane and wall-parallel plane by a plane PIV and a Stereo-PIV systems. The two Nd:Yag laser systems and three CCD cameras were synchronized to obtain instantaneous velocity fields at the same time. To avoid optical noise at the crossing line by the two laser light sheets, a new optical arrangement using polarization was applied. The obtained velocity fields show the existence of hairpin packet structure vividly and the idealized hairpin vortex signature is confirmed by experiment. Two counter-rotating vortex pair which reflects the cutting plane of hairpin legs are found both side of a strong streaky structure when the wall-normal plane cuts the hairpin head.

• 한국전자파학회논문지
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• 제23권3호
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• pp.335-342
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• 2012

저항성 격막을 이용하여 높은 격리도 특성의 Ka-대역 WR-28 도파관 전력합성기를 설계 및 제작하였다. 개발된 도파관 전력합성기는 E-plane T-junction에 슬릿을 만들어 TaN 박막 공정으로 제작된 저항성 격막을 도파관에 결합한 구조이다. 제작된 도파관 전력합성기는 -20 dB 이하의 입출력 임피던스 정합 특성을 보였으며, 0.1 dB 이하의 삽입 손실 특성을 보였다. 또한, 격리도 특성은 거의 전 대역에서 20 dB 이상의 값을 보였으며, 37 GHz 이하에서는 25 dB 이상의 특성을 보여주었다. 입력 포트 상호간의 크기 및 위상 불균형은 각각 0.1 dB와 2.5도 이하의 우수한 특성이 측정되었다.

• 한국전자파학회논문지
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• 제21권7호
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• pp.769-777
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• 2010

본 논문에서는 모서리 접지면 슬롯과 PIN 다이오드를 이용하여 2.4 GHz에서 활용 가능한 편파 변환 특성의 마이크로스트립 패치 안테나를 제안하였다. 제안된 안테나는 정사각형 구조의 마이크로스트립 패치와 접지면에 위치한 두 쌍의 슬롯과 PIN 다이오드로 이루어져 있다. 제안된 안테나에서는 PIN 다이오드의 스위칭 특성을 이용하여 접지면 슬롯의 전기적 길이를 조정하였고, 이를 통해 선형 편파와 좌회전 편파, 우회전 편파 간의 변환 을 구현하였다. 또한 DC 바이어스 회로로 인한 접지면의 분리를 통해서 안테나는 크기 감소 효과를 얻었다. 안테나의 설계 주파수는 2.4 GHz이며, 선형 편파로 동작할 때에는 15 dB의 반사 손실과 59 MHz의 임피던스 대역폭을 가지고, 좌회전 원형 편파와 우회전 원형 편파시 각각 1.17 dB, 1.67 dB의 최소 축비 특성과 28 MHz, 32 MHz의 3-dB 축비 대역폭을 가진다.