• 소음진동
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• 제11권2호
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• pp.241-248
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• 2001

The present paper describes experimental and computational work to augment the magnitude of the impulsive wave. An experiment was performed using a simple shock tube with an open end and numerical calculations were carried out to solve the unsteady, axisymmetric, inviscid, compressible governing equations. The control strategy applied was to alter the exit geometry of a straight tube to a sudden enlargement tube and a flare tube. The effects of the configurations of the tube exit on the magnitude of the impulsive wave were investigated over the range of the weak shock Mach number from 1.01 to 1.10. The results obtained were compared to those of the straight tube tests. The numerical result predicted the magnitude of the experimented impulsive waves with a good accuracy. The present passive control technique enabled the magnitude of the impulsive wave to augment by about 23 percent, compared to that of the straight tube of no control.

• 대한조선학회논문집
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• 제57권2호
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• pp.96-103
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• 2020

The new geometric disturbance is proposed to control the flow around the bluff body. The new geometry is characterized by the variable pitch which is applied on the Helically Elliptic Twisted (HET) cylinder. The performance of the HTE geometry as a biomimetic passive flow control was confirmed by Jung and Yoon (2014). The Large Eddy Simulation (LES) is used for the evaluation of the flow control performance of the Variable Pitch HTE (VPHTE) cylinder at Reynolds number (Re) of 3000 corresponding to the subcritical regime. The circular and HTE cylinders are also considered to compare the performance of the VPHTE cylinder at the same Re. The VPHTE cylinder gives the smallest values of the force coefficients than the circular and HTE cylinders. The drag and lift coefficients of the VPHTE cylinder are about 15.2% and 94.0% lower than those of the circular cylinder, respectively. Especially, the VPHTE cylinder achieves about 2.3% and 30.0% reduction of the drag coefficient and the root mean square of the lift coefficient than the HTE cylinder, respectively. Furthermore, The VPHTE cylinder forms more elongated and stabilized separated shear layer than the circular cylinder, which supports the reduction of the force coefficients.

• 한국생산제조학회지
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• 제21권1호
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• pp.161-166
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• 2012

Intravenous (IV) injection is widely used to supply Ringer solution directly into a vein in hospital. Generally, a passive injection method has been used, which causes the inconsistent flow rate of fluid and inappropriate control of injection time by a patient. It leads to an unnecessary nurse's overwork and decrement of IV injection's effect. To solve these problems, flow control infusion pumps have been developed. But because of relatively heavy weight and high price, its usage has been limited. In the present study, a new automatic IV injection system is developed. It is installed with a small pressing mechanism driven by a small electric motor to regulate the flow rate by pressing tube. Proportional integral derivative (PID) feedback control algorithm is applied to control the electric motor. The system is smaller in size and uses lower power than the existing commercial product. The newly developed system is also installed with networking capability, which enables monitoring the status of several automatic IV injection system at the same time.

• 한국추진공학회지
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• 제13권5호
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• pp.41-47
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• 2009

2차원 초음속 공동유동에서 발생하는 압력진동을 제어하기 위한 목적으로, 본 연구에서는 수치해석적 연구를 수행하였다. 본 계산에서는 압력진동을 제어하기 위하여 보조공동의 형상을 변화시켰으며, 유동의 마하수를 1.50, 1.83 그리고 2.50로 변화시켰다. 그 결과, 보조공동은 압력진동을 상당히 감소시켰으며, 압력진동의 제어효과는 유동의 마하수와 보조공동의 상세형상에 크게 의존함을 알았다.

• 한국자동차공학회논문집
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• 제7권8호
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• pp.190-198
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• 1999

Continuously controlled semi-active suspension system may improve ride and handling properties. Here, as a mechanism to control the fluid flow solenoid valve mechanism is introduced and added to the basic passive damper to create damping forces of the shock absorbers. The system may produce continuously controlled damping forces in both solenoid valve only and combination with passive shock absorber including fluid flow is studied, and then the combined model is added to the full vehicle model to evaluate its ride and handling performance. Finally, the simulation results are compared to the vehicle models having similar suspension system.

• 해양환경안전학회:학술대회논문집
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• 해양환경안전학회 2006년도 추계학술발표회
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• pp.265-269
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• 2006

파랑에 의한 선박의 횡동요를 방지하는 감요장치는 크게 수동식과 능동식 으로 분류할 수 있으며 수동형 감요수조는 선박에서 가장 널리 사용되고 있다. 이 연구에서는 감요장치의 하부덕트유동에 관한 기초연구로서 덕트의 제어 댐퍼와 유입부의 유통에 대해 입자영상 유속측정장치를 이용하여 속도벡터분포에 관한 정량적인 데이터를 확보하였다. 그 결과 실험관 벽면에서 측정 된 압력의 분포는 디스크가 전개 상태인 0 도에서 45도까지는 입구 압력은 일정한 상태로 거의 변화하지 않았으나 약 60도 이상에서부터 압력 상승과 점차 급격한 변동현상이 나타났다.

• 한국가시화정보학회지
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• 제18권1호
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• pp.59-66
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• 2020

In the present study, we experimentally investigated the flow around a circular cylinder with axially arranged holes (AAH). The wind-tunnel experiment was performed at Re = 3.2 × 10⁴ while varying the angle of attack (α) from 0° to 90°. At low α, the passive jet from the AAH pushes near wake to the downstream, increasing the wake formation length. On the other hand, at high α, blowing and suction through AAH occurs alternatively, rather decreasing the wake formation length. The passive jet generated by AAH can effectively control not only the wake where AAH is located, but also the wake between holes. As a result, the AAH reduce the drag on the cylinder up to 23.8% at low α but rather increase the drag at high α, as compared to that on a smooth cylinder.

• Advances in aircraft and spacecraft science
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• 제3권3호
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• pp.271-298
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• 2016

In this paper, we study a problem of passive suppression of helicopter Ground Resonance (GR) using a single degree freedom Nonlinear Energy Sink (NES), GR is a dynamic instability involving the coupling of the blades motion in the rotational plane (i.e. the lag motion) and the helicopter fuselage motion. A reduced linear system reproducing GR instability is used. It is obtained using successively Coleman transformation and binormal transformation. The analysis of the steadystate responses of this model is performed when a NES is attached on the helicopter fuselage. The NES involves an essential cubic restoring force and a linear damping force. The analysis is achieved applying complexification-averaging method. The resulting slow-flow model is finally analyzed using multiple scale approach. Four steady-state responses corresponding to complete suppression, partial suppression through strongly modulated response, partial suppression through periodic response and no suppression of the GR are highlighted. An algorithm based on simple criterions is developed to predict these steady-state response regimes. Numerical simulations of the complete system confirm this analysis of the slow-flow dynamics. A parametric analysis of the influence of the NES damping coefficient and the rotor speed on the response regime is finally proposed.

• 한국항공우주학회지
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• 제32권1호
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• pp.13-21
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• 2004

• 한국항공우주학회지
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• 제32권5호
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• pp.10-17
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• 2004

본 연구에서는 헬리콥터의 전진비행성능 향상에 필수적인 로터블레이드의 동적실속성능을 향상시키기 위한 수동제어기법에 대한 연구를 수행하였다. 로터블레이드의 동적실속성능을 향상시키기 위해서는 블레이드 익형에 발생하는 유동박리에 대한 제어를 통해 양력 특성과 피칭모멘트 특성을 동시에 향상시켜야만 한다. 본 연구에서는 실제구현이 용이한 고정 앞전Droop과 Gurney 플랩을 심한 동적실속영역에 대해 동시에 적용하여 기존의 동적실속 제어기법에 비해서 탁월한 양력성능 향상 및 피칭 모멘트 성능 향상을 얻을 수 있음을 확인하였다.