• Journal of Aerospace System Engineering
• /
• v.4 no.2
• /
• pp.21-25
• /
• 2010

Fatigue properties of composite materials are extremely important to design durable and reliable helicopter rotor blades. However, it is very difficult to apply conventional fatigue test loads in short period. Therefore, accelerating test speed and facilitating spectrum load realization are required. In this study, we have developed a fatigue testing method that uses a resonance of simply supported beam type blade specimen. This test consists in exciting the blade specimen with a frequency that corresponds to its natural frequency. In that case, the test specimen similar to a beam fixed between two pivot points starts vibrating and is significantly deformed. Resonant fatigue tests were performed by changing exciting vertical amplitude and frequency, and S-N curves of each composite materials were successfully obtained.

• Proceedings of the Korean Vacuum Society Conference
• /
• 2015.08a
• /
• pp.140.2-140.2
• /
• 2015

낮은 압력의 평판형 유도 결합 플라즈마 (Inductively Coupled Plasma, ICP)에서 챔버 높이를 바꾸면서 전자 에너지 확률 함수 (Electron Energy Probability Function, EEPF)를 측정하였다. 측정된 전자 에너지 확률 함수에서 기울기가 평평한 부분이 관찰됐고, 이러한 전자 에너지 분포함수의 평평한 부분은 챔버 높이를 증가함에 따라 높은 전자 에너지로 옮겨졌다. 이러한 현상을 분석하기 위해서 2차원 비충돌 가열 메커니즘이 포함된 유도 결합 플라즈마 모델로부터 전자 에너지 확산 계수와 이론적인 전자 에너지 확률 함수를 구하여 실험 결과와 비교하였다. 이를 통하여, 측정된 전자 에너지 확률 함수의 평평한 부분은 전자 튕김 공진 (electron bounce resonance)에 의한 것임을 알 수 있었다.

• Proceedings of the KSME Conference
• /
• 2001.06d
• /
• pp.890-895
• /
• 2001

Pressure resonance frequency that is caused in the combustion chamber can be interpreted to acoustic analysis. Until now the pressure resonance has been assumed and calculated to a disc type combustion chamber that neglected the combustion chamber height because the knock occurs near the TDC(top dead center). In this research FEM(fine element method) has been used to calculate the pressure resonance frequency inside the experimental engine combustion. The reduce error of the resonance frequency obtained by FEM has decreased about 50% compared to the calculation of Draper's equation. Due to the asymmetry in the shape of the combustion chamber that was neglected in Draper's equation we could find out that a new resonance frequency could be generated. To make the experimental results equal we could know that the speed of sound that satisfies Draper's equation was selected 13% higher than all the pent-roof type combustion considered.

• Proceedings of the KSME Conference
• /
• 2001.06d
• /
• pp.483-488
• /
• 2001

In the present study a numerical simulation is performed on a natural convection inside a square cavity with a vibrating wall. The study has been conducted varying the heat transfer rate, wall excitation frequency and also the orientation of the cavity. The temperature and velocities inside the cavity was observed and also, the heat transfer coefficients on the heating wall was seen. From the results, it can be seen that the temperature inside the cavity decreases when excited with the proper frequency and the heat transfer coefficient increased with cavity inclination angle, ${\theta}$. It is also found from the results that flow resonance is occurred near the inclination angle ${\theta}=90^{\circ}$.

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.22 no.5
• /
• pp.573-583
• /
• 1998

Effects of the oscillating incoming flow on vortex shedding and lock-on behind a square cylinder are investigated using numerical simulations at a Reynolds number of 100. Vortex shedding occurred at low forcing frequencies of the incoming flow similar to the natural vortex shedding. As the forcing frequency further increases, the shedding frequency decreases to the half of the forcing freqnency. For a sufficiently large frequency, vortex shedding returns to the natural vortex shedding irrespective of the forcing amplitude. Also, the lock-on region becomes wider with higher forcing amplitudes. The phase diagram between the drag and lift shows a simple periodic behavior in the lock-on region, while a complicated periodic phase relation is observed when there is no lock-on.

• The Journal of Engineering Geology
• /
• v.11 no.1
• /
• pp.25-35
• /
• 2001

For the ground resrxmse analysis, both in-situ and laboratory testing techniques such as downhole, SASW, resonant column and torsional shear tests were perlormed for Hong-Seong area. The grOlmd upper 30m is classified as SD since it has an average shear wave velocity as 209m/s. The response specLrums obtained by site-specific analyses generally satisfied the seismic code, but near the resonance period the motion was evaluated to be higher than the code.

• Proceedings of the KIEE Conference
• /
• 2011.07a
• /
• pp.768-769
• /
• 2011

대용량 수도사업장 고압(6.6[kV]) 비접지 방식의 전력계통 사고는 3상 단락에 비해 1선 지락 사고가 대부분을 차지하고 있다. 1선 지락사고 발생 시 건전상 상전압이 $\surd$3배 상승하고, 공진현상 발생으로 수십배의 전압상승도 일어날 수 있으므로 운전 중인 전력기기 보호를 위해 신속한 지락점 제거가 필요하다. 그러므로 본고에서는 A,B 사업장 펌프기동반의 지락사고 발생을 분석하여 이를 토대로 비접지 계통의 지락보호협조에 대하여 학습하고자 한다.

• The Journal of the Acoustical Society of Korea
• /
• v.12 no.1
• /
• pp.12-19
• /
• 1993

진동시험 동안 구조물은 진동시험기로부터 높은 진동에너지를 받게 되는데 공급되는 에너지를 시험물에 전달하기 위해서는 시험물에 따라 다양한 종류의 진동시험치구가 필요하게 된다. 이중에서 T-형상 진동시험치구는 진동시험축에 대해 3방향으로 시험물을 설치할 수 있고, 형상이 간단하며, 또한 값이 저렴하므로 많은 설계자들은 T-형상 치구를 설계하여 사용한다. 그러나 이 치구는 수직판이 어떤 주파수에서 평판처럼 공진현상을 일으키기 때문에 동역학적으로 설계하기가 어렵다. 본 논문에서는 진동시험치구의 기능을 향상시키기 위해 모우드 시험(Model Testing)기법을 사용하는 방법과 시험결과를 근거로 설계변경을 위해 수직보강판, 수평보강판, 그리고 천연 고무패드를 사용하여 이것들이 치구의 동특성에 미치는 영향을 기술하며 그 결과를 치구설계 때 응용 가능하도록 한다.

• Journal of Astronomy and Space Sciences
• /
• v.20 no.4
• /
• pp.351-358
• /
• 2003

The global stability of the attitude motion of a spin-stabilized space vehicle is investigated by performing numerical experiment. In the previous study, a stationary solution and a particular resonant condition for a given model were found by using analytical method but failed to represent the system stability over parameter values near and off the stationary points. Accordingly, as an extension of the previous work, this study performs numerical experiment to investigate the stability of the system across the parameter space and determines stable and unstable regions of the design parameters of the system.

• Proceedings of the KIEE Conference
• /
• 1989.07a
• /
• pp.28-30
• /
• 1989

This paper is analyzed the electrical characteristics of the round solid rotor of turbo-generator without damper cage influence the induction generation modes and the torsional interaction modes of the SSR phenomena, and then examines the problem of representing electrical characteristics which is dependent on frequency and different wedge materials. The basic model of turbo-generator used in the field analysis is viewed as 5-regions of different permeability and conductivity characteristics. The analytical method, which is used in this paper is based on solving a boundary value problem involving 3-D fields, and the basic function consists of the 2-D Fourier series.