• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 추계학술대회
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• pp.1466-1471
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• 2004

In this paper, we report the numerical and experimental solutions of the axi-symmetric flows in the axial plane driven by an impingement of fluid from the bottom wall of a circular cylinder. We managed to visualize successfully the flow pattern shown on the vertical plane through the container axis. The numerical results are not show to compare well with the experimental results for the case of the Rossby number 3. Because the numerical results calculate on the assumption that vortex flows are axi-symmetric flow on the other hand real experimental results are show asymmetric flow. The numerical solutions reveal that inertial oscillation plays an important role at small Rossby numbers, or at a larger background rotation.

• Structural Engineering and Mechanics
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• 제6권6호
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• pp.613-632
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• 1998

A coupling system for a structure accelerating through a fluid is considered which is composed of the structure and the fluid in a finite surrounding volume. Based on the variational principle, the finite element equations of hydrodynamic pressure and structural elastic vibration are deduced. A numerical method is given for the dynamic character and response of the structure which takes the coupled fluid into account. The effect of axial inertial forces on the dynamic character and response of rapidly accelerating structures is also considered.

• 한국추진공학회지
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• 제8권3호
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• pp.17-26
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• 2004

본 연구에서 동력 전달 시스템은 분리 축 방식의 가스 터빈 엔진의 축 동력을 발전기 전력으로 변환하여, 이것을 프로펠러를 구동하는 추력 모터에 공급하는 방식으로 구성되어있다. 여기에 사용된 가스 터빈 엔진은 엔진 축 마력 317shp(236kw)을 약110kw (147shp)으로 플랫 레이팅(flat rating) 하여 운용한다. 본 시험 장치의 엔진은 가스 터빈엔진 출력축과 발전기 사이에 부하 변화 시 댐핑(damping)역할을 할 수 있도록 플라이 휠(flywheel)을 장착하였다. 이 때 플라이휠의 적절한 관성 모멘트가 고려되지 않으면, 발전기와 모터는 부하 상승에 의한 엔진으로부터 요구되는 출력을 얻을 수 없으며, 또한 엔진이 정상적으로 작동하지 않음을 확인할 수 있다. 따라서 제공된 엔진 데이터와 엔진 시험 데이터로부터 동역학적인 천이 효과에 의한 성능 분석을 함으로써 관성 모멘트의 요구 범위를 결정하였다. 재설계한 플라이휠을 장착 시험한 결과, 본 시스템에서 요구한 출력을 얻을 수 있었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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• pp.183-188
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• 2003

본 연구에서는 분리 축 방식의 가스터빈엔진을 축소형 무인 비행선의 발전용 추진시스템으로 활용하기 위해서 분리 축 가스터빈엔진을 발전용으로 개조하였다. 엔진시험을 통해 출력축으로부터 부하를 전달할 때, 요구되는 구동로터의 조건을 분석하였다. 분석한 결과 적절한 댐핑(damping)역할을 하는 장치가 필요함을 알 수 있다. 따라서 댐퍼 역할을 하는 flywheel의 관성모멘트의 변화를 고려하여 정량화하는 방법을 선택하였다. 적합한 flywheel의 관성모멘트를 장착 할 수 없는 경우에는 엔진으로부터 요구되는 출력을 얻을 수 없으며, 또한 엔진 시험중 불안정성이 초래함을 확인할 수 있었다. 엔진시험에 의한 데이터 분석으로부터 동역학적인 천이효과에 의한 성능을 통해 관성모멘트의 요구범위를 확인 할 수 있었다. 재설계한 Flywheel을 장착하여 시험한 결과 정상적인 엔진작동으로부터 추진 시스템에 요구되는 출력을 얻을 수 있었다. 엔진 시스템의 천이작동모드에서는 Fuel flow schedule 대한 엔진 응답이 제어 시스템에 제공되기 때문에, 제어시스템 설계와 천이작동모드는 충분히 고려해야 할 것이다.

• Structural Engineering and Mechanics
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• 제66권5호
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• pp.649-663
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• 2018

The scaled boundary finite element method is extended to evaluate the dynamic stress intensity factors and T-stress with a numerical procedure based on the improved continued-fraction. The improved continued-fraction approach for the dynamic stiffness matrix is introduced to represent the inertial effect at high frequencies, which leads to numerically better conditioned matrices. After separating the singular stress term from other high order terms, the internal displacements can be obtained by numerical integration and no mesh refinement is needed around the crack tip. The condition numbers of coefficient matrix of the improved method are much smaller than that of the original method, which shows that the improved algorithm can obtain well-conditioned coefficient matrices, and the efficiency of the solution process and its stability can be significantly improved. Several numerical examples are presented to demonstrate the increased robustness and efficiency of the proposed method in both homogeneous and bimaterial crack problems.

• Computers and Concrete
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• 제15권4호
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• pp.515-545
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• 2015

The paper presents results of FE simulations of the strain-rate sensitive concrete behaviour under dynamic loading at the macroscopic level. To take the loading velocity effect into account, viscosity, stress modifications and inertial effects were included into a rate-independent elasto-plastic formulation. In addition, a decrease of the material stiffness was considered for a very high loading velocity to simulate fragmentation. In order to ensure the mesh-independence and to properly reproduce strain localization in the entire range of loading velocities, a constitutive formulation was enhanced by a characteristic length of micro-structure using a non-local theory. Numerical results were compared with corresponding laboratory tests and available analytical formulae.

• 한국정밀공학회지
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• 제14권2호
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• pp.13-22
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• 1997

Strapdown inertial navigation system(SDINS) is a navigational instruments necessary to guide and con- trol a free vehicle. In this study, an error analysis of mechanical parts is carried out for manufacturing a dynamically tuned gyroscope. The errors usually come from the tolerance in machining and assembly. In the error analysis, a criterion to be considered during designing and manufacturing is proposed by quanti- tatively analyzing the effect of DTG performance by tolerances. The theory of dynamic balancing is deduced and unbalance is reduced through experiment.

• 한국자동차공학회논문집
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• 제19권2호
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• pp.133-141
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• 2011

The effect of payload on fuel consumption and emission of light duty freight truck during acceleration driving has been analyzed. Running tests were carried out with various payload conditions on chassis dynamometer. A typical driving pattern for urban cities was used. Real time emission measurement systems for gaseous and soot emission were utilized to investigate the real time dynamic of fuel use and exhaust emissions. It was observed that fuel use and pollutant emissions were increased as payload was increased. Under the same payload condition, the increased amount of acceleration driving is much higher than that of steady state driving. The results demonstrated the advantages of eco-driving, which is an environmentally friendly driving manner, could be emphasized in heavier payload condition. Inertial tractive power was introduced for considering the parameters affecting emission during acceleration driving, which are speed, acceleration and payload. Fuel use and emission in various driving conditions were expressed as functions of inertial tractive power. The estimated result by these functions well predicted measured result within 10 % deviation.

• Computers and Concrete
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• 제22권6호
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• pp.515-525
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• 2018

This paper presents a numerical study on the performance of reinforced concrete (RC) bridge structures subjected to heavy goods vehicle (HGV) collision. The objectives of this study are to investigate the dynamic response and failure modes of different types of bridges under impact loading as well as to give an insight into the simplified methods for modeling bridge structures. For this purpose, detailed finite-element models of HGV and bridges are established and verified against the full-scale collision experiment and a recent traffic accident. An intensive parametric study with the consideration of vehicle weight, vehicle velocity, structural type, simplified methods for modeling bridges is conducted; then the failure mode, impact force, deformation and internal force distribution of the validated bridge models are discussed. It is observed that the structural type has a significant effect on the force-transferring mechanism, failure mode and dynamic response of bridge structures, thus it should be considered in the anti-impact design of bridge structures. The impact force of HGV is mainly determined by the impact weight, impact velocity and contact interface, rather than the simplification of the superstructure. Furthermore, to reduce the modeling and computing cost, it is suggested to utilize the simplified bridge model considering the inertial effect of the superstructure to evaluate the structural impact behavior within a reasonable precision range.

• 한국소음진동공학회논문집
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• 제21권9호
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• pp.813-819
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• 2011

This paper predicted nonlinear dynamic responses of a cantilevered carbon nanotube(CNT) resonator incorporating the electrostatic forces and van der Waals interactions between the CNT cantilever and ground plane. The structural model of CNT includes geometric and inertial nonlinearities to investigate various phenomena of nonlinear responses of the CNT due to the electrostatic excitation. In order to solve this problem, we used Galerkin's approximation and the numerical integration techniques. As a result, the CNT nano-resonator shows the softening effect through saddle-node bifurcation near primary resonance frequency with increasing the applied AC and DC voltages. Also we can predict nonlinear secondary resonances such as superharmonic and subharmonic resonances. The superharmonic resonance of the nano-resonator is influenced by applied AC voltage. The period-doubling bifurcation leads to the subharmonic resonance which occurs when the nano-resonator is actuated by electrostatic forces as parametric excitation.