• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1998.04a
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• pp.465-470
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• 1998

A cross-flow fan often generates discrete noise call blade passing frequency tones. Several methods have been investigated to reduce this BPF noise, where the random distribution of blades is the most promising one. A simple and effective algorithm to determine a random distribution of blades is proposed which considers fan. performance as well as noise characteristics. The proposed method is verified by a simple numerical model and is applied in manufacturing cross-flow fan samples. Also some experiments are carried out and the experimental results are analyzed.

• Geotechnical Engineering
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• v.2 no.2
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• pp.29-36
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• 1986

In this study, a random vibration technique to anaiyze the vertical vibration of rigid circular footings on sand whose material properties are not previously determind is proposed. Total of 11 circular model footings varing mass ratio and radius are constructed for the vibration experim eat and the elastic half space is represented by compacted sand layer From the random vibration experiments, it is found that the technique suggested in this study gives more accurate prediction of circular footing behavior under vertical vibration than the simplified analog which assumes the subsoils as elastic half space. The predicted resonant frequene iris agree very well with the measured values from the slnusoidal vibration experiments. The ratio of the predicted resonant amplitudes to the measured values vary between 0.5 and 1,35 for the site used for the vibration experiments in this study.

• Geotechnical Engineering
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• v.11 no.4
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• pp.37-48
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• 1995

The dynamic behavior of dry sand under different vibration conditions is studied through laboratory experiments. Sinusoidal and random vibration experiments of sand are carried out in vertical direction under various surcharge loads. Five different sand samples are selected for the azperiment. They are composed of four different -size samples of particles and one sample which is simulated the field condition. In case of sinusoidal vibration, the change in relative density is measured with acceleration levels. To produce an acceleration, the vibration amplitude is maintained within the range of 0.4mm~0.6mm and the vibration frequency is changed within the range of 3Hz~40Hz. In case of random vibration, the combined sinusoidal acceleration is produced by a random vibration generator and the change in relative density is measured by an accelerometer. Based on the experimental results, it is found that the sandy soil is compacted to 94%~99% of relative density by vertical acceleration and the peak acceleration producing the maximum relative density is proportional to the difference between maximum and minimum void ratios. It is also found that the effect of surcharge loading : the greater the surcharge loading, the larger the change in relative density and the greater the acceleration required to change the relative density.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.8
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• pp.627-638
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• 2017

Expecting fatigue life of mounted radar in aircraft is very important when designing, because the mounted radar in aircraft is exposed to long-term external random vibration. Among the methods of predicting the fatigue life, Fatigue analysis method in frequency domain has continuously been proposed in this field. In this paper, four fatigue analysis methods in frequency domain, which are widely used, have been selected and compared with the results for Specimen fatigue test. As a result, Dirlik and Benascicutti-Tovo methods have been matched better with fatigue analysis in time domain than the method in frequency method through the comparison between the fatigue analysis method in time domain and the method in frequency domain by conducting the specimen fatigue test with strain gage. Based on the results of the specimen fatigue test, We have conducted fatigue analysis of mounted radar in aircraft with Dirlik and Benasciutti-Tovo methods in the finite element model, and confirmed that the required life was satisfying.

• Journal of KSNVE
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• v.8 no.4
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• pp.690-699
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• 1998

This paper discusses the techniques, procedures and the results of the ground vibration test(GVT) performed on the development aircraft and the simple procedure of FE model updating technique from the GVT results. The GVT was carried out using random excitation technique with MIMO(Multi-Input-Multi-Output) data acquistion method, and taking full advantage of poly-reference global parameter estimation technique to identify the vibration modes. In dynamic FE modeling, the aircraft was represented by beam elements and all dynamic analysis was performed using MSC/NASTRAN for this model. In updating procedure, the stiffness of the beam model was adjusted iteratively so as to get the natural frequencies and mode shapes close to the GVT results.

• Proceedings of the KIEE Conference
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• 2015.07a
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• pp.1227-1228
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• 2015

본 연구에서는 기계적 충격 방식을 통한 주파수 상향방식을 이용하여 저주파 진동원으로부터 충분한 에너지를 수확할 수 있는 압전 구동 방식의 광대역 에너지 수확 소자를 제작하고 평가하였다. 유연한 외팔보의 진동으로 인한 기계적 충격은 압전 외팔보에 큰 두 번째 힘을 전달한다. 변형률이 커지고 주파수 상향방식을 사용한 결과로 출력 전력과 동작 주파수의 대역폭 또한 향상되었다. 제작된 에너지 수확소자의 질량체 비율은 ${\mu}=5.8$, 스토퍼의 거리는 d = 0.5 mm이며, 17 Hz의 주파수, $30k{\Omega}$의 최적 부하저항에서 $449{\mu}W$의 최대 피크 전력을 전달하였다. 또한 1 g로 가진하였을 때 11 Hz부터 28 Hz의 주파수 대역에서 동작이 가능하였고, 저주파수의 무작위 진동에서도 효율적으로 에너지 수확이 가능하다는 것을 입증하였다.

• Journal of Korean Academy of Nursing
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• v.28 no.3
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• pp.591-601
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• 1998

미숙아에 있어 주로 표면활성제의 부족으로 인한 호흡곤란증은 미숙아 사망의 주원인이 된다. 호흡곤란증의 치료목적은 적절한 환기를 통해 체내 산소화를 유지시키는 것이다. 인공호흡기 치료를 받는 미숙아에게 필수적인 간호중재인 기관지 흡인술은 그 효과를 극대화하기 위해 흉곽진동법과 같이 사용될 수도 있다. 그러나 미숙아를 대상으로 하는 흉곽진동법은 그 중재의 안전성이나 효과에 대한 과학적 검증 없이 시행되고 있는 실정이다. 이에 본 연구는 호흡곤란증 미숙아에 있어 기관지 흡인술 이전에 행하여지는 흉곽진동법이 산소화와 기관지 분비물에 미치는 영향을 연구하기 위해 실시되었다. 이를 위해 20명의 호흡곤란증 미숙아를 대상으로 대상자내 반복실험연구가 설계되었다. 독립변수는 기관지흡인술이전에 흉곽진동이고 종속 변수는 산소 포화도, 심박동수, 그리고 기관지 분비물의 양이었다. 각 대상자는 무작위 순서에 따라 한번은 흉곽진동없이 흡인을, 나머지 한번은 흉곽진동과 흡인의 두 가지 형태의 흡인을 경험 하였다. 연구 결과, 기관지 흡인술이전에 흉곽진동을 실시하든, 안하든 산소포화도와 심박동수의 변화양상에는 차이가 없었다. 그러나, 융곽진동법을 실시한 경우가 실시안한 경우에 비해 더 많은 양의 기관지 분비물을 흡인하였다. 이는 기관지 흡인술 이전에 실시하는 흉곽진동법이 미숙아의 체내에 부가적 산소소모를 초래하지 않는 반면, 기도로부터 더 많은 분비물을 흡인하는데 효과적임을 시사한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.50 no.5
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• pp.317-323
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• 2022

In this paper, a deep neural network(DNN) model for predicting the vibration characteristics of the composite rotor blade with c-spar cross section was developed. Herein, the present DNN model is defined by using the natural frequencies obtained through the in-house code based on the nonlinear co-rotational(CR) shell element. For the present DNN model, the accuracy of the model was evaluated via the data with a random distribution of thickness and a tendency to decrease in thickness along the blade span.

• Journal of Korea Society of Industrial Information Systems
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• v.12 no.1
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• pp.101-107
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• 2007

In this paper, we proposed an stable optical security system using interferometer and cascaded phase keys. For the encryption process, a BPCGH(binary phase computer generated hologram) that reconstructs the origial image is designed, using an iterative algorithm and the resulting hologram is regarded as the image to be encrypted. The BPCGH is encrypted through the exclusive-OR operation with the random generated phase key image. For the decryption process, we cascade the encrypted image and phase key image and interfere with reference wave. Then decrypted hologram image is transformed into phase information. Finally, the origianl image is recovered by an inverse Fourier transformation of the phase information. During this process, interference intensity is very sensitive to external vibrations. a stable interference pattern is obtained using self-pumped phase-conjugate minor made of the photorefractive material. In the proposed security system, without a random generated key image, the original image can not be recovered. And we recover another hologram pattern according to the key images, so can be used an authorized system.

• Journal of the Korean Society of Manufacturing Process Engineers
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• v.21 no.1
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• pp.73-80
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• 2022

Sensors are applied to small aviation platforms for various purposes. Radio frequency (RF) antennas, which are representative sensors, are available in many forms but require the application of slot array RF antennas to ensure high performance and designation. Slot RF array antennas are applied to dip brazing techniques, but the yield and production time are determined by the proficiency of production personnel in a labor-intensive form. Unmanned aerial vehicles or drones, which are representative small aviation platforms, are continuously exposed to various random vibrations because propellers and multiple power sources are used in them. In this study, the fatigue life of slot array RF antennas applied with additive manufacturing was evaluated through the cumulative damage method (Miner's rule) in a vibration environment with a small aviation platform. For the evaluation, an S N curve obtained from a fatigue strength test was used.