• Smart Structures and Systems
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• 제5권6호
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• pp.645-662
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• 2009

Adaptive wings are capable of properly modifying their shape depending on the current aerodynamic conditions, in order to improve the overall performance of a flying vehicle. In this paper is presented the concept design of a small-scale compliant wing rib whose outline may be distorted in order to switch from an aerodynamic profile to another. The distortion loads are induced by shape memory alloy actuators placed within the frame of a wing section whose elastic response is predicted by the matrix method with beam formulation. Genetic optimization is used to find a wing rib structure (corresponding to the first airfoil) able to properly deforms itself when loaded by the SMA-induced forces, becoming as close as possible to the desired target shape (second airfoil). An experimental validation of the design procedure is also carried out with reference to a simplified structure layout.

• 설비공학논문집
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• 제14권3호
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• pp.199-205
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• 2002

In this paper, the optimum shape and arrangement of ribs in the channel of a plate heat exchanger are studied. The following dimensionless geometric parameters of ribs are selected as design variables: rib height ($H_R$), angle of attack ($\beta$), rib pitch ($P_R$), rib distance (L) and aspect ratio of rib (AR). The optimization is performed by minimizing the objective function consisting of the Nusselt number and the friction factor. The optimal values of design variables are as follows: $H_R$=0.263, $\beta$=0.290, $P_R$=3.142, L: 3.954, AR=0.342. The pressure drop and the heat transfer of the optimum model, compared to those of the reference model, are increased by 15.1% and 41.6%, respectively.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집B
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• pp.241-247
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• 2001

A comparison of fully developed heat transfer and friction factor characteristics has been made in rectangular ducts with ones roughened by five different shapes. The effects of rib shape geometries and Reynolds number are examined. The rib height-to-duct hydraulic diameter, pitch-to-height ratio, and aspect ratio of channel width to height are fixed at e/De=0.0476, P/e=8, and W/H=2.33, respectively. To understand the mechanisms of the heat transfer enhancements, the measurements of the friction factors are also conducted in the smooth and rough channels. The data indicates that the triangular type rib has a substantially higher heat transfer performance than any other ones in the range we studied.

• 설비공학논문집
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• 제13권5호
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• pp.341-347
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• 2001

A comparison of fully developed heat transfer and friction factor characteristics has been made in rectangular ducts with ones roughened by five different shapes. The effects of rib shape geometries and Reynolds number are examined. The rib height-to-duct hydraulic diameter, pitch-to height ratio, and aspect ratio of channel width to height are fixed at $e$/De=0.0476, P/$e$=8, and W/H=2.33, respectively. To understand the mechanisms of the heat transfer enhancements, the measurements of the friction factors are also conducted in the smooth and rough channels. The data indicates that the triangular type rib has a substantially higher heat transfer performance than any other ones in the range we studied.

• 한국공간구조학회논문집
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• 제23권4호
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• pp.27-34
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• 2023

In this study, the seismic response characteristics of the three analysis model with or without TMD were investigated to find out the effective dome shape. The three analysis models are rib type, lattice type and geodesic type dome structure composed of space frame. The maximum vertical and horizontal displacements were evaluated at 1/4 point of the span by applying the resonance harmonic load and historical earthquake loads (El Centro, Kobe, Northridge earthquakes). The study of the effective TMD installation position for the dome structure shows that seismic response control was effective when eight TMDs were installed in all types of analysis model. The investigation of the efficiency of TMD according to dome shape presents that lattice dome and geodesic dome show excellent control performance, while rib dome shows different control performance depending on the historical seismic loads. Therefore, lattice and geodesic types are desirable for seismic response reduction using TMD compared to rib type.

• 조명전기설비학회논문지
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• 제16권2호
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• pp.59-64
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• 2002

본 논문에서는 전계해석을 통하여 금속성 파티클이 GIS 스페이서의 여러 위치에 부차되었을 경우 립이 파괴전압특성에 미치는 영향을 분석하였다. 또한, 립-스페이서의 여러 위치에 금속성 파티클을 부착하고 립의 모양, 길이, 두께 등의 변화에 따라 얻은 파괴진압특성 실험결과를 전계해석의 결과와 비교·검토하였다. 전계해석의 결과 립의 연면에서의 전계집중이 다른 부분에 비하며 완화되어 절연파괴시 발생된 스트리머의 진전이 억제될 수 있다는 것을 알 수 있었으며, 실험을 통하여 파괴전압이 상승된다는 것을 확인할 수 있었다. 또한 립의 길이와 두께 등에 따라서도 파괴전압 특성이 달라짐을 알 수 있었다. 또한 립의 끝단을 라운드 처리함으로써 파괴전압 특성을 더욱 향상시킬 수 있음을 전계해석과 실험을 통하여 알 수 있었다.

• 대한기계학회논문집
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• 제16권8호
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• pp.1468-1484
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• 1992

본 연구에서는 유한요소법을 이용해서 초기형상을 결정하는 새로운 방법으로 서 전방 투사법을 제안하고자 한다. 전방 투사법으로서 선형 보간을 이용한 방법과 소성 문제의 물리적인 특성을 고려하여 퍼지 로직을 도입한 퍼지시스템을 개발하려 한 다. 선형보간을 이용한 전방투사법은 임의의 초기 형상에 대한 유한 요소 해석 결과 얻어진 최종 형상에서의 미 충만 부피를 선형 보간하여 초기 형상에 적용함으로서 최 적 초기 형상을 결정하는 방법이다. 그러나 미 충만 부피의 변화가 미소할때에는 쉽 게 최적 초기 값을 찾지 못하는 경우가 발생하므로 유동 특성을 고려한 퍼지 로직을 구성하여 퍼지 시스템을 개발하였다. 이 방법을 리브-웨브(rbi-web)형태의 축대칭 단조 문제에 적용하고 유한 요소법에 의한 해석중 격자 재구성의 필요에 의해 단위체 격자 재구성법을 이용한다. 결정해야될 초기 형상의 변수로서는 형상비(aspect ra- tio=높이/지름)을 고려하기로 한다.

• 동력기계공학회지
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• 제5권2호
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• pp.30-35
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• 2001

A comparison of fully developed heat transfer and friction factor characteristics has been made in rectangular ducts with one wall roughened by five different shapes. The effects of rib shape geometries and Reynolds number are examined. The rib height-to-duct hydraulic diameter, pitch-to-height ratio, and aspect ratio of channel width to height are fixed at $e/D_e=0.0476$, P/e=8, and W/H=2.33, respectively. To understand the mechanisms of the heat transfer enhancements, the measurements of the friction factors are also conducted in the smooth and rough channels. The data indicate that the triangular type rib has a substantially higher efficiency index than any other ones in the range we studied.

• Journal of Mechanical Science and Technology
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• 제16권4호
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• pp.549-556
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• 2002

An investigation on the fully developed heat transfer and friction factor characteristics has been made in rectangular ducts with one-side roughened by five different shapes. The effects of rib shape geometries as well as Reynolds numbers are examined. The rib height-to-duct hydraulic diameter, pitch-to-height ratio, and aspect ratio of channel width to height are fixed at e/De=0.0476, P/e=8, and W/H=2.33, respectively. To understand the characteristics of heat transfer enhancements, the friction factors are also measured. The data indicates that the triangular type rib has a substantially higher heat transfer performance than any other ones.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 1996년도 추계학술대회논문집
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• pp.113-121
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• 1996

AI7075 alloy has been used for aircraft components since it has the advantage of high strength, high toughness, and high corrosion resistance. Many airframe components consist of various combinations of rib-web structure. In this study, various process paramenters such as die design, lubricant, ram speed, forging temperature have been investigated using the experiment and F.E.M. simulation to develop the precision forging technology for AI7075. When lubricant is applied to both material and die, shear friction factor is 0.1 which shows best effect of lubricant. It is specific corner radius of die that minimized forging load regarding process conditions, especially according to the ratio of the width of rib and web. In conclusion, optimum corner radius is 2~3mm when the width of rib and web is 3mm and 20mm respectively.