• 한국전자파학회논문지
• /
• 제27권6호
• /
• pp.521-530
• /
• 2016

기상레이다는 전자기파를 대기 중에 방사하여 목표물에 부딪혀서 되돌아오는 후방산란 신호를 수신하는 기상장비이다. 기상청의 기상레이다는 도플러 관측 기능을 가지고 있기 때문에 목표물의 시선속도를 산출할 수 있다. 그러나 기상레이다의 넓은 관측 반경을 확보하려면 관측 속도 범위가 작아져 이를 넘어서는 시선속도는 접힘 현상이 발생한다. 따라서 최대 관측 반경을 유지한 채 관측 속도 범위를 넓히기 위해서는 high PRF와 low PRF 두 개의 서로 다른 PRF로 신호를 송 수신하는 dual PRF(Pulse Repetition Frequency) 모드 기능을 이용해야 한다. Dual PRF 모드를 이용하면 high와 low PRF로 관측된 두 최대 속도의 최소공배수만큼 관측 속도 범위를 넓힐 수 있다. 이를 위해 본 연구에서는 high PRF와 low PRF로 관측된 시선속도의 차이값과 이에 대한 오차를 고려한 분류 기준을 만들고, 분류된 영역별로 보정 인자를 산출하여 시선속도 펼침을 수행하는 시선속도 접힘 풀기 알고리즘을 개발하였다. 이를 용인테스트베드레이다에 적용한 결과, 기존에 산출되는 시선속도보다 개선된 성능을 보였다.

• 한국수자원학회논문집
• /
• 제34권6호
• /
• pp.641-649
• /
• 2001

본 연구에서는 군말뚝 교각 주위에서의 세굴특성을 실험을 통하여 파악하였다. 실험은 4개, 9개, 15개, 35개의 파일로 구성된 군말뚝에 대해 수행하여 파일수, 유속, 접근각에 따른 세굴형상, 최대세굴심의 깊이 및 위치의 변화를 살펴보았다. 실험결과에 의하면, 4개 및 9개로 구성된 군말뚝의 경우 유속비와 상관없이 단일교각의 최대세굴심과 흡사하였고, 15개와 35개로 구성된 군말뚝의 경우 유속비가 증가함에 따라 최대세굴심도 급격히 증가하여 단일교각 세굴심 의 약 2.2배 증가함을 알 수 있었다. 또한 세굴형태는 말뚝간격이 조밀해질수록 원형의 세굴공이 중첩되어 전체적으로 직사각형의 형태를 띠는 것으로 나타났다. 75개의 파일로 구성된 군말뚝에 대한 접근각의 영향을 살펴본 결과 세굴심은 접근각이 35$^{\circ}$에서 최대가 되었으며 이때의 세굴공은 대각선 방향으로 형성됨을 알 수 있었다.

• 한국시뮬레이션학회논문지
• /
• 제8권4호
• /
• pp.25-31
• /
• 1999

To analyze the impulsive response of a motorcycle helmet, a simulation is performed using the finite element method. Based upon the simulation result, an equivalent one degree of freedom vibrational system is adapted, and transient impulsive responses are analysed to investigate the influence of engineering parameters such as damping, natural frequency, and impact velocity on the impulsive response of the helmet. Maximum gravitational acceleration reduces as the damping factor value increases. When the damping factor value is around 0.6 or larger, the maximum acceleration does not change. With respect to the natural frequency and the impact velocity, it increases linearly. The relationship between head injury criterion(HIC) and maximum gravitational acceleration is also presented. The scheme of this study is expected to be utilized to economize the design process of high quality motorcycle helmets.

• 한국정밀공학회지
• /
• 제15권6호
• /
• pp.97-106
• /
• 1998

In this Paper, a fuel minimizing closed loop explicit inertial guidance algorithm for orbit injection of a rocket is developed. In the formulation, the fuel burning rate and magnitude of thrust are assumed constant. The motion of rocket is assumed to be subject to the average inverse-square gravity, but negligible effects from atmosphere. The optimum thrust angle to obtain a given velocity vector in the shortest time with minimizing fuel consumption is first determined, and then the additive thrust angle for targeting the final position vector is determined by using Pontryagin's maximum principle. To establish real time processing, many algorithms of onboard guidance software are simplified. The explicit guidance algorithm is simulated on the 2nd-stage flight of the N-1 rocket developed in Japan. The results show that the explicit guidance algorithm works well in the presence of the maximum $\pm$10% initial velocity and altitude errors, and exhibits better performance than the open-loop program guidance. The effects of the guidance cycle time are also examined.

• 드라이브 ㆍ 컨트롤
• /
• 제20권4호
• /
• pp.9-16
• /
• 2023

This paper analyzed a drainage tower used to drain water in flooded areas. Multi-body dynamics simulation was used to analyze the dynamic behavior of the drainage tower. Structural analysis, flexible-body dynamic analysis, and rigid body dynamic analysis were done to study the maximum Von-Mises stress of the drainage tower. The results showed that the maximum Von-Mises stress occurs at the turn table, and it decreases when the angle of the boom is increased. Also, the rate of the change of angle affects the maximum stress so that the maximum stress changes more when the angular velocity of the boom increases. Based on the rigid body dynamic analysis and the theoretical analysis results, the centrifugal force from the angular velocity makes the difference in the maximum stress at the turn table because of the difference in their direction. Consequently, it was concluded that the centrifugal force should be considered when designing construction machinerythat can rotate.

• 한국의류학회지
• /
• 제22권5호
• /
• pp.565-574
• /
• 1998

The purpose of the study was to determine the effect of air velocity on the thermal resistance of wool ensembles. Three suits for men with different weaving structure and density were made with the same design and size for the study. In addition, Y-shirt, underwear, and socks were prepared for constructing the ensembles. Thermal insulation of air layer and 3 ensembles were measured by using thermal manikin in environmental chamber controlled at 2$0^{\circ}C$ and 65% RH with various air velocity. The results were as follows: 1. Thermal resistance of air layer was 0.079 m2.$^{\circ}C$/W with no air velocity(less than 0.2m/sec). 2. Thermal resistance of air layer decreased with increasing the air velocity rapidly. When the air velocity was 0.25 and 2.89 m/sec, the decreasing rate was 15% and 61%, respectively compared with no air velocity. 3. While there was little difference among the effective thermal insulation of 3 ensembles having different weaving structure and density with no air velocity, there was sharp difference among them when the air velocity increased. That is, the decreasing rate of effective thermal insulation of the ensemble which has higher air permeability was higher. 4. The decreasing rates of the effective thermal resistances of plain, twill and satin ensemble were 61, 54, and 49%, respectively when the air velocity was 2.89 m/sec which was a maximum air velocity in this study.

• 한국지반신소재학회논문집
• /
• 제5권1호
• /
• pp.25-32
• /
• 2006

방조제 공사는 바다를 막아 바닷물의 흐름을 차단해가는 과정으로 육상공사와는 달리 수심이 깊고 파랑이 심한 바다에서 이루어지는 공사이기 때문에 축조재료의 유실이 많고 심할 경우 방조제가 붕괴되는 위험이 큰 공사이다. 특히, 방조제의 끝막이 단면은 대규모 사석과 돌망태 등을 이용하여 시공하므로, 구성 재료가 불규칙하고 간극이 크기 때문에 일반적인 지반내의 침투흐름보다 상당히 빠른 침투가 발생된다. 본 연구에서는 방조제 끝막이 후 축조된 사석단면과 후속공정을 통하여 축조되는 방조제단면에 대한 실내 침투모형시험을 수행하여 침투거동을 예측 및 분석하였다. 다양한 조위변화를 재현하여 근고공 필터매트 시공에 따른 사석단면내의 유속변화, 침윤선 분포 등을 계측하여 침투거동을 분석하였다. 실내 침투모형시험 결과, 끝막이 사석단면의 침투유속은 최대 1.7m/sec 발생하였으며, 근고공 필터매트 시공에 따라 최대 침투유속이 23.7% 감소하였다.

• 한국연소학회:학술대회논문집
• /
• 한국연소학회 2004년도 제29회 KOSCI SYMPOSIUM 논문집
• /
• pp.62-69
• /
• 2004

Zone conditional formulations for the Reynolds average reaction progress variable are used to derive an asymptotic expression for turbulent burning velocity. New DNS runs are performed for validation in a statistically one dimensional steady state configuration. Parametric study is performed with respect to turbulent intensity, integral length scale, density ratio and laminar flame speed. Results show good agreement between DNS results and the asymptotic expression in terms of measured maximum flame surface density and estimated turbulent diffusivity in unburned gas.

• 한국연소학회지
• /
• 제9권4호
• /
• pp.1-8
• /
• 2004

Zone conditional formulation for the Reynolds average reaction progress variable is used to derive an asymptotic expression for turbulent burning velocity. New DNS runs are performed for validation in a statistically one dimensional steady state configuration. Parametric study is performed with respect to turbulent intensity, integral length scale, density ratio and laminar flame speed. Results show good agreement between DNS results and the asymptotic expression in terms of measured maximum flame surface density and estimated turbulent diffusivity in unburned gas.

• 대한의용생체공학회:학술대회논문집
• /
• 대한의용생체공학회 1994년도 춘계학술대회
• /
• pp.111-114
• /
• 1994

Three component velocity measurements with a refractive index-matching technique was used to investigate the flow characteristics in the atrio-pulmomnary (AP) Fontan connection under the steady flow condition. A strong swirl was observed in the extra-cardiac conduit and the main pulmonary artery (MPA). Maximum velocity magnitude in the MPA was about 0.8 m/s near the posterior wall at 6 liter/min. Swirling motion of the flow as well as geometric abnormalities of the connection are important factors in energy loss across Fontan connections.