• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2007년도 춘계학술대회논문집
• /
• pp.85-92
• /
• 2007

This paper presents a design optimization of a new Advanced Active Blade Twist (AATR-II) blade incorporating single crystal Macro Fiber Composites (MFC) and conducts vibratory loads reduction analysis using an obtained optimal blade configuration. Due to the high actuation performance of the single crystal MFC, the AATR blade may reduce the helicopter vibration more efficiently even with a lower input-voltage as compared with the previous ATR blades. The design optimization provides the optimal cross-sectional configuration to maximize the tip twist actuation when a certain input-voltage is given. In order to maintain the properties of the original ATR blade, various constraints and bounds are considered for the design variables selected. After the design optimization is completed successfully, vibratory load reduction analysis of the optimized AATR-II blade in forward flight condition is conducted. The numerical result shows that the hub vibratory loads are reduced significantly although 20% input-voltage of the original ATR blade is used.

• 항공우주시스템공학회지
• /
• 제10권4호
• /
• pp.50-58
• /
• 2016

선행 연구 개발을 통하여 장기 체공 태양광 무인기 복합재 날개의 경량화는 매우 중요한 요소임을 확인하였다. 날개 외피의 좌굴 방지와 비틀림 방지 역할을 하는 구조물인 리브는 날개의 구성 요소 중에 필수적이다. 본 연구는 최적의 복합재 리브를 설계, 제작하기 위하여 복합소재의 이방성 특성을 고려한 다양한 적층 패턴 적용 및 형상에 대하여 리브를 제작하였고. MSC. Patran/Nastran을 이용한 유한요소 해석을 통하여 최대 하중 및 변위 형상을 확인하였으며, 구조 시험을 통하여 측정된 시험 결과를 바탕으로 최적의 리브를 제시하였다.

• 한국소음진동공학회논문집
• /
• 제15권7호
• /
• pp.799-805
• /
• 2005

This paper describes the development process of high stiffness body for ride and handling performance. High stiffness and light weight vehicle is a major target in the refinement of Passenger cars to meet customers' contradictable requirements between ride and handling performance and fuel economy This paper describes the analysis approach process for high stiffness body through the data level of body stiffness. According to the frequency band. we can suggest the design guideline about lg cornering static stiffness, torsional and lateral stiffness, body attachment stiffness. The ride and handling characteristic of a vehicle Is significantly affected by vibration transferred to the body through the chassis mounting points from front and rear suspension. It is known that body attachment stiffness is an important factor of ride and handling performance improvement. And high stiffness helps to improve the flexibility of bushing rate tuning between handling and road noise. It makes possible to design the good handling performance vehicle and save vehicles to be used in tests by using mother car at initial design stage. These improvements can lead to shortening the time needed to develop better vehicles.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 1995년도 추계학술대회논문집; 한국종합전시장, 24 Nov. 1995
• /
• pp.185-190
• /
• 1995

In recent years, many researcher have been interested in the stability of a thin beam. Among them, Pai and Nayfeh[1] had investigated the nonplanar motion of the cantilever beam under lateral base excitation and chaotic motion, but this study is associated with internal resonance, i.e. one to one resonance. Also Cusumano[2] had made an experiment on a thin beam, called Elastica, under bending loads. In this experiment, he had shown that there exists out-of-plane motion, involving the bending and the torsional mode. Pak et al.[3] verified the validity of Cusumano's experimental works theoretically and defined the existence of Non-Local Mode(NLM), which is came out due to the instability of torsional mode and the corresponding aspect of motions by using the Normal Modes. Lee[4] studied on a thin beam under bending loads and investigated the routes to chaos by using forcing amplitude as a control parameter. In this paper, we are interested in the motion of a thin beam under torsional loads. Here the form of force based on the natural forcing function is used. Consequently, it is found that small torsional loads result in instability and in case that the forcing amplitude is increasing gradually, the motion appears in the form of dynamic double potential well, finally leads to complex motion. This phenomenon is investigated through the poincare map and time response. We also check that Harmonic Balance Method(H.B.M.) is a suitable tool to calculate the bifurcated modes.

• 한국세라믹학회지
• /
• 제28권1호
• /
• pp.20-28
• /
• 1991

Fracture of Al2O3 tubes for different loading path under combined tension/torsion was investigated. Macroscopic directions of crack propagation agreed well with the maximum principal stress criterion, independent of the loading path. However, fracture strength from the proportional loading test($\tau$/$\sigma$= constant) showed either strengthening or weakening compared to that from uniaxial tension, depending on the ratio $\tau$/$\sigma$. The Weibull theory was capable to predict the strengthening of fracture strength in pure torsion, but not the weakening in the proportional loading condition. The strengthening or weakening of fracture strength in the proportional loading condition was explained by the effect of shear stresses in the plane of randomly oriented microdefects. Finally, a new empirical fracture criterion was proposed. This criterion is based on a mixed mode fracture criterion and experimental data for fracture of Al2O3 tubes under combined tension/torsion. The proposed fracture criterion agreed well with experimental data for both macroscopic directions of crack propagation and fracture strengths.

• 대한기계학회논문집A
• /
• 제21권6호
• /
• pp.971-980
• /
• 1997

This study is to investigate the stiffness degradation of a composite laminated panel including transverse matrix cracks subjected to bending and twisting moments. Micromechanics theory on the composite material is derived by introducing crack density. Iterative numerical scheme is developed to calculate the degraded composite stiffness which has nonlinear relation due to the crack density. The finite element method is used for structural analysis of the composite panel. Structural responses of the composite panel are examined for various laminated angles and crack density under the bending and twisting moments. Also, the effect of crack opening and closing is considered in the examination. It is realized that the matrix cracks may cause severe stiffness reduction and should be considered in the composite laminated panel.

• 전산구조공학
• /
• 제10권2호
• /
• pp.203-211
• /
• 1997

고층건물의 설계에 있어서 지진보다 바람에 의한 영향이 더욱 크므로 바람에 의한 건물의 안전성과 거주성등을 검토하는 것이 중요하다. 이러한 내풍해석은 모형 실험을 통하여 그 결과를 예측할 수 있으나 본 연구에서는 수치해석의 모형 개발에 중점을 두어 변동 풍하중의 3차원 모델과 건물 평면의 비대칭성을 고려하여 동조질량감쇠기를 설치하였을 때의 건물의 진동 성능을 분석하고 있다. 건물의 질량과 강성중심이 일치하지 않아 횡변위와 비틀림이 연계되는 102층의 건물을 예로 들어 내풍해석 및 동조질량감쇠기를 설치하였을 때 진동제어 해석을 수행하여 건물의 변위와 가속도의 평균응답을 구하여 결과를 비교하였다.

• 한국안전학회지
• /
• 제17권4호
• /
• pp.189-195
• /
• 2002

I-단면 곡선보 (curved beam)의 모멘트 하중 하에서 비틀림(warping)을 포함한 평면외 (out-of-plane)의 좌굴을 미분구적법 (DQM)을 이용하여 해석하였다. 다양한 경계조건(boundary conditions) 및 굽힘각(opening angles)에 따른 임계모멘트 (critical moments)를 계산하고, DQM의 해석결과는 해석적 해답 (exact solution) 과 비교 분석하였다. DQM은 적은 요소(grid points)를 사용하여 정확한 해석결과를 보여주었고, 두 경계조건 (고정-고정, 고정-단순지지)하에서 새로운 결과 또한 제시하였다.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2004년도 추계학술대회논문집
• /
• pp.358-361
• /
• 2004

This paper describes the development process of high stiffness body for ride and handling performance. High stiffness and light weight vehicle is a major target in the refinement of passenger cars to meet customers' contradictable requirements between ride and handling performance and fuel economy. This paper describes the analysis approach process for high stiffness body through the data level of body stiffness. According to the frequency band, we can suggest the design guideline about Is cornering static stiffness, torsional and lateral stiffness, body attachment stiffness. The ride and handling characteristic of a vehicle is significantly affected by vibration transferred to the body through the chassis mounting points from front and rear suspension. It is known that body attachment stiffness is an important factor of ride and handling performance improvement. And high stiffness helps to improve the flexibility of bushing rate tuning between Handling and road noise. It makes it possible to design the good handling performance vehicle at initial design stage and save vehicles to be used in tests by using mother car at initial design stage. These improvements can lead to shortening the time needed to develop better vehicles.

• Composites Research
• /
• 제30권5호
• /
• pp.280-287
• /
• 2017

복합재 후퇴익은 비행 중 굽힘 하중 외에도 비틀림 하중을 받아 복잡한 변형이 발생할 수 있다. 따라서 복잡한 변형이 나타나는 복합재 후퇴익의 구조 건전성 평가를 위해 복합재 후퇴익 구조물의 변위 예측이 요구된다. 날개의 변위 예측은 변위와 변형률 관계를 통해 예측할 수 있지만 후퇴익의 복잡한 변형으로 고정단 부근의 변형률 분포는 복잡하게 나타나기 때문에 일부 위치의 변형률 센서만으로 변형률을 측정하면 변위 예측의 오차가 발생할 수 있다. 본 논문에서는 복잡한 변형률 분포를 고려한 평판 형태의 복합재 후퇴익의 변위를 예측하는 연구를 수행하였다. 유한요소 해석을 통해 변형률 측정 지점을 선정하였다. 측정 지점의 변형률을 이용하여 예측한 변위는 해석에서 계산된 변위와 잘 일치하였으며, 실험을 통하여 검증하였다.