• 제목/요약/키워드: lifting surface method

검색결과 77건 처리시간 0.021초

수정진동자에 의한 LB초박막의 평가 (Evaluation of Langmuir-Blodgett Ultra-thin Films by using a Quartz Crystal)

  • 최용성;박옥순;김철홍;장상목;권영수
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 1992년도 춘계학술대회 논문집
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    • pp.39-41
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    • 1992
  • The characteristics of LB ultra-thin film multi-layers were evaluated by the AT-cut quartz crystal. Cholesterol and phosphatidyl choline LB multi-layers were deposited on the surface of quartz crystal by using vertical lifting method and horizontal lifting method. There was good relationship between deposition ratio and frequency shift, and the frequency was more stable at the case of horizontal lifting method to the vertical lifting method.

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비선형 와류격자법을 이용한 작은 종횡비 날개의 고받음각 및 지면효과 후류 특성 분석 (Wake Characteristics of High Angle of Attack and Ground Effect for Low Aspect Ratio Wings using NLVLM)

  • 이세욱
    • 융복합기술연구소 논문집
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    • 제4권1호
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    • pp.37-41
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    • 2014
  • For the analysis of lifting surface at high angle of attack, a Nonlinear Vortex Lattice Method(NLVLM) was used. The NLVLM is intented to compute the interactions between lifting surfaces and separated vertical flow. The lifting surfaces are represented by a lattice of discrete vortex rings. And wakes are represented by families of non-lintersecting, semi-infinite vortex line segments. The image method also used to analyze the ground effect. It is found that vortex lines separated from lifting surfaces represent the separated flows successfully. Although the present method is applied for the rectangular wing and delta wing, extensions can be possible for the arbitrary lifting surfaces. The Present results show good agreement with experimental data.

Optimization of the Propeller Steady Performance Behind Wake Field

  • Lee, Wang-Soo;Choi, Young-Dal;Kim, Gun-Do;Moon, Il-Sung;Lee, Chang-Sup
    • Journal of Ship and Ocean Technology
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    • 제11권2호
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    • pp.10-25
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    • 2007
  • With the sharp increase of the oil price, the issue of the energy saving requires even higher propulsive efficiency of the propellers. Traditionally the propellers have been designed with the criteria such as that of Lerbs optimum based on the lifting line theory and the empirical formulae of Lerbs and van Manen giving relations of the wake pitch with the wake non-uniformity. With the aid of the high speed computer, it is now possible to apply the time-consuming iterative approaches for the solution of the lifting surface problems. In this paper we formulate the variational problem to optimize the efficiency of the propeller operating in the given ship wake using the lifting surface method. The variational formulation relating the spanwise circulation distribution with the propulsive efficiency to be maximized is however non-linear in circulation distribution functions, thus the iterative method is applied to the quasi-linearized equations. The blade shape design also requires the iterative procedures, because the shape of the blade which is represented by the lifting surface is unknown a priori. The numerical code was validated with the DTNSRDC propeller 4119 which is well-known to be optimum in uniform inflow condition. In addition existing (well-designed) commercial propellers were selected and compared with the results of the open water tests and the self-propulsion tests.

Horn Type 타(舵)와 한쌍(雙)의 타(舵)의 타직압력(舵直壓力) 계산(計算)에 관한 연구(硏究) (Calculation of the Rudder Normal Force for a Horn Type Rudder and Twin Rudder)

  • 이승건
    • 대한조선학회지
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    • 제27권4호
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    • pp.27-31
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    • 1990
  • 양력면(揚力面)의 양력계산(揚力計算)에 흔히 쓰이고 있는 방법(方法)을 크게 나누면 Vortex Lattice 법(法)과 Mode Function법(法)이 있다. 잘 알려진 것 처럼, Vortex Lattice법(法)은 해(解)의 수렴성(收斂性)은 좋으나 계산시간(計算時間)이 많이 걸리는 문제점(問題點)이 있고, Mode Function법(法)은 계산시간(計算時間)은 짧으나 해(解)가 특이(特異)해 지는 경우가 있다. 그러므로 본(本) 논문(論文)에서는 양방법(兩方法)의 장점(長點)들을 살리도록, 양력면(揚力面)을 Span 방향(方向)으로 분할(分割)하고 각(各) Strip Mode Function을 사용하여 Vortex를 분포(分布)시켜, 양력면이론(揚力面理論)으로 양력(揚力)을 계산(計算)하였다. 우선 Horn Type의 반균형타(半均衡舵)에 본(本) 계산법(計算法)을 적용(適用)하여 타직압력(舵直壓力)을 계산(計算)하고 타(舵) 단독시험(單獨試驗)을 병행(竝行)하여 계산법(計算法)의 유용성(有用性)을 검증(檢證)하였다. 그 결과(結果), Stall과 같은 비선형적(非線形的) 유체현상(流體現象)이 일어나지 않는 한(限), 본(本) 계산법(計算法)은 유용(有用)하다는 결론(結論)을 얻었다. 끝으로, 본(本) 계산법(計算法)을 평행(平行)하게 늘어선 한척(隻)의 장방형타(長方形舵)에 적용(適用)하여 두 타(舵) 사이의 상호간섭(相互干涉)도 계산(計算)하였다.

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sEMG 분석을 이용한 높이 들어올리기 자세에서의 신체적 작업부하의 정량적 평가방법 개발 (Evaluation Method of Physical Workload in Overhead Lifting Posture Using Surface EMG Analysis)

  • 이영진;지영준
    • 대한의용생체공학회:의공학회지
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    • 제32권4호
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    • pp.328-335
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    • 2011
  • For human factor engineering and wearable robot design, the quantitative assessment of physical workload is needed. Through measuring the surface EMG (sEMG) and analysis, the physical workload in overhead lifting posture is presented in quantitative manner. By normalizing sEMG activities with maximal voluntary contraction (MVC), the inter-subject variability is reduced. In all muscles, %MVC increased as the weight of lifting object increases. In anterior deltoid muscle, the %MVC was 3-4 times higher than the other muscles which imply that this muscle performs the major role in the overhead lifting posture. In fatigue analysis, %MVC and the mean frequency in muscle of anterior deltoid changed markedly when compared with other muscles. Through the suggested procedures and analysis, the physical workload for a specific posture can be represented in quantitative way but the clinical meaning for the value should be investigated further.

Frequency Domain Analysis of Lifting Problems with Explicit Kutta Condition

  • Kim, Jong-Un;Kim, Gun-Do;Lee, Chang-Sup
    • Journal of Ship and Ocean Technology
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    • 제7권3호
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    • pp.34-55
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    • 2003
  • Explicit Kutta condition approximation, proved useful in existing time-domain solver of the unsteady propeller problem, requires a specified functional behavior of the vorticity in space near the trailing edge. In this paper, the strength of the discrete vortices is controlled to have a specified behavior in space in the frequency domain approach. A new formulation is introduced and is implemented for analysis of a lifting surface of a rectangular planform. Sample computations carried out according to the new formulation compares well with that of existing unsteady lifting problem in the time domain.

Aerodynamic Design and Analysis of a Propeller for a Micro Air Vehicle

  • Cho Lee-Sang;Yoon Jae-Min;Han Cheol-Heui;Cho Jin-Soo
    • Journal of Mechanical Science and Technology
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    • 제20권10호
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    • pp.1753-1764
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    • 2006
  • A U-80 propeller and its modified version, U-75 propeller, are used for a micro air vehicle. The performance characteristics of a U-80 propeller and a U-75 propeller have not much known in the published literature. Thus, their aerodynamic characteristics are investigated using a lifting surface numerical method. The lifting surface method is validated by comparing computed results with measured data in a wind tunnel. From the computed results, it is found that the U-75 propeller produces larger thrust with higher efficiency than the U-80 propeller. To enhance the performance of these propellers, a new propeller is designed by following the sequential design procedures with the design parameters such as hub-tip ratio, maximum camber and its position, and chord length distribution along the radial direction. The performance of the designed propeller is shown to be improved much comparing with those of both the U-80 and U-75 propellers.

프리캐스트 콘크리트 포장 시공 시 최적 슬래브 리프팅 위치 (Optimum Slab-Lifting Positions for Precast Concrete Pavement Construction)

  • 김성민;조병휘;한승환
    • 한국도로학회논문집
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    • 제9권2호
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    • pp.27-37
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    • 2007
  • 본 연구는 프리캐스트 콘크리트 포장 시공을 위하여 공장에서 미리 제작된 콘크리트 슬래브를 리프팅을 할 때 리프팅 위치에 따른 슬래브의 응력변화를 기준으로 슬래브의 손상을 최소화할 수 있는 가장 안전한 최적 리프팅 지점을 선정하기 위하여 수행되었다. 리프팅 시 슬래브의 응력분포를 분석하기 위하여 유한요소법을 이용한 모델을 사용하였으며 슬래브 규격은 시험시공에서 사용한 크기를 적용하였다. 리프팅은 항상 슬래브의 수직방향으로 수행하지는 않기 때문에 수직으로 리프팅 하였을 때와 $60^{\circ},\;30^{\circ}$로 경사각을 주어 리프팅 하였을 때의 응력변화 특성을 분석하였다. 또한 리프팅 지점은 항상 슬래브의 중간 깊이인 중립축의 위치가 아니기 때문에 중립축으로부터 7.5cm. 15cm만큼 수직편심을 주어 리프팅하였을 때의 응력변화 특성도 분석하였다. 그리고 실제 시공 시 지점부분에 보강을 하는 것을 염두하여 지점부 응력집중현상을 무시한 경우와 보강이 없을 경우의 응력집중현상을 고려한 경우로 나누어 분석하였다. 이러한 해석을 통해 리프팅 경사각과 편심에 따른 최적 리프팅 위치를 선정하였으며 미국의 PCI기준과도 비교 분석하였다.

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Gang-Form 떨어짐재해 예방관리를 위한 인양고리 최적화에 관한 연구 (Gang - form or run for Accident Prevention lifting lug A Study on Optimization)

  • 정현옥;강경식
    • 대한안전경영과학회지
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    • 제16권3호
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    • pp.231-237
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    • 2014
  • Construction of the external wall framing using construction Gang-Form withstand the load of a full lift safety is very important in lifting rings can be a lot of Gang-Form is now fixed in the manner that you are welding and applied, but this study is based on the safety of the lifting ring to seek improvements were bolt type fixing method applied to the bonding type were part of the lifting ring in a manner fixed to the concrete surface and was applied in consideration of safety.

Hybrid RANS and Potential Based Numerical Simulation for Self-Propulsion Performances of the Practical Container Ship

  • Kim, Jin;Kim, Kwang-Soo;Kim, Gun-Do;Park, Il-Ryong;Van, Suak-Ho
    • Journal of Ship and Ocean Technology
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    • 제10권4호
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    • pp.1-11
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    • 2006
  • The finite volume based multi-block RANS code, WAVIS developed at MOERI is applied to the numerical self-propulsion test. WAVIS uses the cell-centered finite volume method for discretization of the governing equations. The realizable $k-{\epsilon}$ turbulence model with a wall function is employed for the turbulence closure. The free surface is captured with the two-phase level set method and body forces are used to model the effects of a propeller without resolving the detail blade flow. The propeller forces are obtained using an unsteady lifting surface method based on potential flow theory. The numerical procedure followed the self-propulsion model experiment based on the 1978 ITTC performance prediction method. The self-propulsion point is obtained iteratively through balancing the propeller thrust, the ship hull resistance and towing force that is correction for Reynolds number difference between the model and full scale. The unsteady lifting surface code is also iterated until the propeller induced velocity is converged in order to obtain the propeller force. The self-propulsion characteristics such as thrust deduction, wake fraction, propeller efficiency, and hull efficiency are compared with the experimental data of the practical container ship. The present paper shows that hybrid RANS and potential flow based numerical method is promising to predict the self-propulsion parameters of practical ships as a useful tool for the hull form and propeller design.