• 제목/요약/키워드: Cylindrical Rear Surface

검색결과 4건 처리시간 0.017초

원통형 배면체를 갖는 PZT 트랜스듀서의 특성평가 (Characteristics Evaluation for a PZT Transducer with a Cylindrical Rear Surface)

  • 김동현;한진호;양정원;김무준;하강렬
    • The Journal of the Acoustical Society of Korea
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    • 제26권1E호
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    • pp.14-20
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    • 2007
  • The characteristics of a PZT transducer with a cylindrical rear surface were investigated theoretically and experimentally. The transducer was assumed as a set of finite rectangular ceramic elements for applying the staircase model to the theoretical analysis and the KLM equivalent circuit model was modified for analyzing its electric impedance and pulse-echo response. All results were compared with those of a conventional plane transducer which has a constant thickness of average value for the cylindrical arc. It was noted that the transducer with a cylindrical rear surface has several subsidiary resonant frequencies which are able to widen bandwidth.

Effect of the curved vane on the hydraulic response of the bridge pier

  • Qasim, Rafi M.;Jabbar, Tahseen A.;Faisa, Safaa H.
    • Ocean Systems Engineering
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    • 제12권3호
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    • pp.335-358
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    • 2022
  • Hydrodynamic field alteration around a cylindrical pier using a curved vane is numerically investigated. The curved vane with various angles ranged from 10 to 220 degree is placed at the upstream of the cylindrical pier. Laminar flow is adopted in order to perform the steady-state analysis. It is found that the flow separation leads to the formation of four bubbles depending on the value of the curved vane angle. Two bubbles are located in the region between the rear of the curved vane and the leading surface of the cylindrical pier, while the remaining two bubbles are located at the wake zone behind the cylindrical pier. Numerical analysis is performed to reveal the hydrodynamic field and influence of curved vane on the formation and evolution of the bubbles. It is found that the center and size of the bubble depend mainly on the value of the curved vane angle. It is observed that the flow velocity vector shows clearly the alteration in the flow velocity direction especially at the leading surface and rear surface of the curved vane owing to the occurrence of flow separation and flow dissipation along the circumference of the vane.

직교유동 내에 놓인 수평 실린더에서 서리 생성에 관한 실험적 연구 (An experimental study of frost forming on the horizontal cylinder under cross flow)

  • 이윤빈;노승탁
    • 설비공학논문집
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    • 제11권4호
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    • pp.448-456
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    • 1999
  • Variations of thickness and effective thermal conductivity of frost forming on the horizontal] cylinder with respect to time were measured under cross flow. The local heat flux around the cylinder was determined by measuring the radial temperature distribution in the cylinder having small holes drilled axially in which T-type thermocouples were inserted, then by using one dimensional cylindrical heat conduction equation. The thickness and the surface temperature of the frost layer around the cylinder were measured periodically while developing the frost. Each experiment was peformed by varying the Reynolds number, the temperature, and the humidity condition. Specially the dew point temperature of the most cases was below the freezing point. Experimental data showed that the frost layers on the front and the rear surface were thicker than those on the top and the bottom one which was near the separation point. The thickness and effective thermal conductivity of the frost layer were affected by inlet air velocity, temperature, and humidity. Moreover, the effective thermal conductivity and the effective thermal resistance increase with respect to time.

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3차원 patched-grid 알고리즘을 이용한 삼각 날개-원통형 동체 형상 전산 해석 (Computational Analysis of the Delta Wing-Cylindrical Body Configuration Using the Three-Dimensional Patched-Grid Algorithm)

  • 박현돈;김영진;박수형
    • 한국항공우주학회지
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    • 제48권2호
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    • pp.109-117
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    • 2020
  • 기존 정렬 격자의 많은 제약 조건들을 완화할 수 있는 patched-grid 알고리즘을 이용하여 효율적으로 정렬 격자계를 구성하였다. EFD-CFD 워크숍의 case 4: 삼각 날개-원통형 동체 형상에 크게 3가지의 접근 방식을 적용하여 기존의 격자 생성 문제점들을 해결하였고, 실험값과 비교하여 검증하였다. 고 받음각 영역에서 표면 압력 분포가 실험값과 다소 차이를 보였다. 마하수의 증가에 따른 피칭 모멘트의 기울기 변화를 분석하였고 이는 tuck under 현상으로 설명할 수 있었다. 초음속 영역에서는 형상 앞에 궁형 충격파가 발생함으로써 삼각익 뒷전까지 양력을 발생시키는 영역이 확장되었다. 또한, 마하수와 받음각에 따라 압력 중심과 무게 중심의 위치를 비교하여 피칭 모멘트의 경향성을 분석하였다.