• 제목/요약/키워드: Shock loss factor

검색결과 27건 처리시간 0.077초

샌드위치 구조를 가지는 복합재의 손실계수 향상을 위한 설계 (Design for Improving the Loss Factor of Composite with Sandwich Structure)

  • 이창민;전관수;강동석;김병준;김종훈;강명환;서영수
    • 한국소음진동공학회논문집
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    • 제26권3호
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    • pp.235-241
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    • 2016
  • Underwater weapon system is required to structurally strong material, since as it is directly exposed to external shock. It should also be using the lightweight material in order to take advantage of buoyancy. Composite materials meet these requirements simultaneously. Particularly in the case of submarine, composite materials are widely used. It is important to have a high strength enough to be able to withstand external shock, but it is also important to attenuate it. In a method for the shock damping, viscoelastic damping materials are inserted between the high strength composite material as a sandwich structure. Shock attenuation can be evaluated in the loss factor. In ASTM(American Society of Testing Materials), evaluation method of the loss factor of cantilever specimens is specified. In this paper, mode tests of the cantilever are performed by the ASTM standard, in order to calculate the loss factor of the viscoelastic damping material by the specified expression. Further, for verifying of the calculated loss factor, mode test of compound beams is carried out. In addition, the characteristics of the material were analyzed the effect on the loss factor.

네트워크형 복층 도로터널 환기에서의 충격 손실 평가를 위한 수치해석적 연구 (Numerical Analysis on the Estimation of Shock Loss for the Ventilation of Network-type Double-deck Road Tunnel)

  • 박상훈;노장훈;김진
    • 터널과지하공간
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    • 제27권3호
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    • pp.132-145
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    • 2017
  • 과거 도로터널 환기에 있어서 충격 손실은 설계에 반영되지 않았지만, 터널 내 네트워크형 구조로 인해 분기 합류부가 존재하는 복층 도로터널에서는 충격 손실에 의한 압력 손실이 크게 발생할 것이다. 이에 본 연구에서는 네트워크형 구조를 가지는 복층 도로터널 최적 환기 설계를 위하여 분기 합류 지점에서 발생하는 충격 손실에 대한 3D 전산유체역학(CFD) 수치해석 연구를 수행한다. 이를 위해 복층 도로터널 표준단면을 적용한 실제 스케일 모델을 활용하여 전산 유체 역학을 수행하였고 다양한 각도와 차도폭에 대한 충격 손실 계수를 도출하여 기존의 설계 값과 비교 분석하였다. 연구 결과, 분기 구간에서는 30도의 분류 각도를 가진 모델의 충격 손실 계수가 높게 측정되었고, 합류 구간에서는 2차선으로 설계된 모델의 충격 손실 계수가 낮게 측정됨을 확인할 수 있었다. 따라서 분기 합류 각도와 차도폭이 충격 손실 산정에 있어서 중요한 설계 요소가 될 수 있으므로 환기기 용량 산정에 있어서 정확한 설계 인자를 제시할 것으로 판단된다. 본 연구는 3D 전산유체역학(CFD)를 활용하여 확폭 교차 유 무에 따른 분기 합류 지점에서의 충격 손실 계수를 도출하고, ASHRAE 설계 값과 결과를 비교 분석하였다. 확폭 구간이 반영되지 않은 모델은 ASHRAE 값에 비해 최대 3배의 충격 손실 값을 확인하였고, 확폭 구간이 반영된 모델은 최대 2배의 값을 확인할 수 있었다.

가압열충격을 고려한 원자로 압력용기의 파괴역학적 해석 (Fracture Mechanics Analysis of a Reactor Pressure Vessel Considering Pressurized Thermal Shock)

  • 박재학;박상윤
    • 한국안전학회지
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    • 제16권4호
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    • pp.29-38
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    • 2001
  • The purpose of this paper is to evaluate the structural integrity of a reactor pressure vessel subjected to the pressurized thermal shock(PTS) during the transient events, such as main steam line break(MSLB) and small break loss of coolant accident(SBLOCA). For postulated surface or subsurface cracks, variation curves of stress intensity factor are obtained by using the three different methods, including ASME section XI code anlysis, the finite element alternating method and the finite element method. From the stress intensity factor curves, the maximum allowable nil-ductility transition temperatures(RT/NDT/) are determined by the tangent criterion and the maximum criterion for various crack configurations and two initial transient events. As a result of the analysis, it is noted that axial cracks have smaller maximum allowable RT$_{NDT}$ values than same-sized circumferential cracks for both the transient events in the case of the tangent criterion. Axial cracks have smaller RT$_{NDT}$ values than same-sized circumferential cracks for MSLB and circumferential cracks have smaller values than axial cracks for SBLOCA in the case of the maximum criterion.

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공동주택에서 완충재를 이용한 바닥충격음 저감 System 연구 (Investigating of a Floor-Impact Isolation System Using Damping Materials In Apartment Buildings)

  • 송희수;정영;정정호;전진용
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 춘계학술대회논문집
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    • pp.499-504
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    • 2004
  • The purpose of this study is to investigate a investigating of a floor-impact isolation system using damping materials in apartment buildings. The stiffness elastic modulus(k) by puls impact forces were calculated loss factor by Hilbert transforms. It is absolved that natural frequency was moved floor shock-absorbing materials and the impact force was reduced by floor panel. The slab was constructed by damping materials. As towards a result, the system showed inverse A 45dB by heavy weight-impact noise and inverse A 52dB by light-impact noise. High frequencies impact-noise can be reduced by upgrading naturial frequency of vibration and noise in the system.

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가압열충격 사고에 대한 원자로 용기의 최대 허용 기준무연성천이온도 (Maximum Allowable $RT_{NDT}$ of Nuclear Reactor Vessel for Pressurized Thermal Shock Accident)

  • 정명조;박윤원;송선호
    • 전산구조공학
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    • 제11권1호
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    • pp.153-160
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    • 1998
  • 본 연구에서는 가압열충격 사고로 소형 냉각재 상실사고를 가정하여 냉각재의 온도와 압력의 이력으로 부터 용기 벽의 온도분포를 구하고, 이로 부터 열응력과 압응력을 해석적으로 구하였다. 또 균열 선단에서의 응력강도계수와 파괴인성치를 ASME코드의 방법을 이용하여 구하였고, 이들을 시간에 따라 비교하여 균열의 진전여부를 평가하였다. 원자로 용기 벽에 존재하는 여러 형태의 균열이 견딜 수 있는 최대 기준무연성천이온도를 결정하였으며 평가 결과에 대하여 고찰하였다.

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초음속 회전익의 앞전 형상이 공력 성능에 미치는 효과에 대한 수치적 연구 (Numerical Study on The Effects of Blade Leading Edge Shape to the Performance of Supersonic Rotors)

  • 박기철
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2001년도 유체기계 연구개발 발표회 논문집
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    • pp.149-155
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    • 2001
  • Recently, it is required to design higher stage pressure ratio compressor while maintaining equal adiabatic efficiency. To increase the stage pressure ratio, blade rotational speed or diffusion factor should be increased. In the case of increasing rotational speed, relative speed of flow at blade leading edge is well supersonic. In supersonic blade, total pressure loss is mainly due to shock wave and blade leading edge thickness should be very thin to minimize the shock wave loss. As a result, the blade is like to be week in terms of mechanical strength and the manufacturing cost is very high because NC machining is necessary. It is also one of big hurdle to overcome to make small compressor. In this paper, the effects of blade leading edge to the performance of supersonic blade In terms of total pressure loss. The efficiency of already known method to make thin blade leading edge from the casted blade with rather thick leading edge thickness is also assessed.

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신규간호사의 전환충격 측정도구 개발 (Development of the Transition Shock Scale for Newly Graduated Nurses)

  • 김은영;여정희;이경임
    • 대한간호학회지
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    • 제47권5호
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    • pp.589-599
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    • 2017
  • Purpose: The purpose of this study was to develop a scale to assess the transition shock experienced by newly graduated nurses, and test the validity and reliability of the scale. Methods: The initial items were identified through a review of literature and in-depth interviews with nine newly graduated nurses. Content validation of the items was evaluated by five nurse professors and three nurses. Participants were 269 newly graduated nurses who worked at six acute care hospitals in Busan, Ulsan, and Yangsan, South Korea. Data were analyzed using item analysis, exploratory and confirmatory factor analysis, criterion related validity, and internal consistency. Results: The final scale consisted of 18 items and six factors (conflict between theory and practice, overwhelming workload, loss of social support, shrinking relationship with co-workers, confusion in professional nursing values, and incongruity in work and personal life), which explained 71.3% of the total variance. The six subscale model was validated by confirmatory factor analysis. Cronbach's alpha for the total items was. 89. Convergent validity was evaluated by analyzing total correlation with burnout (r=.71, p<.001) and turnover intention (t=5.84, p<.001). Conclusion: This scale can be used in the development of nursing interventions to reduce the transition shock experienced by newly graduated nurses.

익렬 위치에 따른 초음속 터빈의 확산 손실에 대한 실험적 연구 (An experimental study on the expansion loss of a supersonic turbine with the cascade position)

  • 조종재;김귀순;정은환
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제27회 추계학술대회논문집
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    • pp.387-392
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    • 2006
  • 본 연구에서는 초음속 충동형 터빈의 유동특성을 알아보기 위해 소형 초음속 풍동을 설계하였다. 실험은 익렬 위치에 따른 초음속 터빈의 유동 특성을 파악하고 확산 손실이 발생하는 특성을 알기 위해 익렬의 위치를 조절해가며 2차원 초음속 노즐과 익렬을 조합하여 실시하였다. Z-type 슐리렌(Schlieren) 시스템을 이용하여 유동을 가시화 하였다. 이러한 실험을 통해 충격파를 포함한 복잡한 유동 형태와 유동박리, 충격파-경계층 상호작용 등을 관찰할 수 있었다.

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충격파 저감을 위한 ER 지능구조물 (ER Smart Structures for Shock Wave Reduction)

  • 김재환;김지선;최승복;김경수
    • 한국소음진동공학회논문집
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    • 제13권9호
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    • pp.679-687
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    • 2003
  • Shock wave reduction in electrorheological(ER) smart structures is studied. ER insert is a composite structure comprising two elastic outer layers between which is sandwiched layer of ER fluid. When a voltage is applied across the outer layers. the shear modulus and the loss factor of the ER fluid are enabled, and thus the dynamic properties of the composite structure is altered. For the shock wave reduction in a hull mount of a submerged structure, ER inserts are made on the hull mount structure. To investigate the ER insert shape. many types of ER insert pattern are considered. Modal test of ER insert structures is performed to obtain the mode shapes, natural frequencies and the acceleration transmissibility. The acceleration transmissibility is reduced at such a frequency region when an electric field is applied. It is observed that the natural frequencies and mode shapes can be tunable by applying electric field. The ER-inserted hull mount is installed in an integrated system and the overall performance of shock wave reduction is tested. The possibility of shock wave reduction in the hull mount is demonstrated.

Deterministic structural and fracture mechanics analyses of reactor pressure vessel for pressurized thermal shock

  • Jhung, M.J.;Park, Y.W.
    • Structural Engineering and Mechanics
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    • 제8권1호
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    • pp.103-118
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    • 1999
  • The structural integrity of the reactor pressure vessel under pressurized thermal shock (PTS) is evaluated in this study. For given material properties and transient histories such as temperature and pressure, the stress distribution is found and stress intensity factors are obtained for a wide range of crack sizes. The stress intensity factors are compared with the fracture toughness to check if cracking is expected to occur during the transient. A round robin problem of the PTS during a small break loss of coolant transient has been analyzed as a part of the international comparative assessment study, and the evaluation results are discussed. The maximum allowable nil-ductility transition temperatures are determined for various crack sizes.