• Journal of Astronomy and Space Sciences
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• v.24 no.3
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• pp.219-226
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• 2007

Among the interplanetary shock (IP shock)s observed by ACE spacecraft at 1AU during 1997 to 2000, we have selected 31 IP shocks which had triggered the interplanetary type II radio bursts detected by the WIND spacecraft while those shocks were leaving the Sun. We compared the observed IP shock propagation speeds and the IP shock transit speeds estimated by time difference between the interplanetary type II radio burst detection and the IP shock observation. Then, we found that the mean acceleration of the IP shocks between the Sun and the Earth is about $-1.02m/sec^2$, which means the deceleration contrary to the positive acceleration predicted by Parker solar wind model. It is also verified that the acceleration of the IP shock does not show any linear correlation with the shock propagation speed and the Mach number of the IP shock.

• The Journal of the Acoustical Society of Korea
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• v.27 no.7
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• pp.333-341
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• 2008

In this paper, a new interpolation model for the head related transfer function (HRTF) was proposed. In the method herein, we assume that the impulse response of the HRTF for each azimuth angle is given by linear interpolation of the time-delayed neighboring impulse responses of HRTFs. The time delay of the HRTF for each azimuth angle is given by sum of the sound wave propagation time from the ears to the sound source, which can be estimated by using azimuth angle, the physical shape of the underlying head and the distance between the head and sound source, and the refinement time yielding the minimum mean square error. Moreover, in the proposed model, the interpolation intervals were not fixed but varied, which were determined by minimizing the total number of HRTFs while the synthesized signals have no perceptual difference from the original signals in terms of sound location. To validate the usefulness of the proposed interpolation model, the proposed model was applied to the several HRTFs that were obtained from one dummy-head and three human heads. We used the HRTFs that have 5 degree azimuth angle resolution at 0 degree elevation (horizontal plane). The experimental results showed that using only $30\sim40%$ of the original HRTFs were sufficient for producing the signals that have no audible differences from the original ones in terms of sound location.

• Proceedings of the Korea Society for Industrial Systems Conference
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• 2000.11a
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• pp.353-356
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• 2000

두 물체의 충격운동량-충격 및 탄성파 발생의 순으로 작용하도록 하면 계 내에서 충돌 후 생기는 운동량의 관성 속도와 충돌기간동안 발생하는 탄성파의 충격에너지 전달속도가 다른 경우가 있다. 이것은 충돌기간동안 총 운동량은 보존되나 선 운동량이 비 보존되는 경우가 있어서 충돌기간동안 비 보존된 내부 운동량의 시간 적분만큼 충돌을 가한 질량중심이 이동했다는 의미이다. 충돌기간동안 충격파는 탄성파에 근사시키고 그것은 군속도에 근사시켜 이론적 근거를 만들고 실험에 의해 확인했다. 폐쇄된 계 내에서 내부에너지를 이용하여 특별한 두 물체의 충돌기간동안 비 보존되는 운동량 때문에 질량중심이 이동되는 것에 대해 해석한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.6
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• pp.587-593
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• 2008

Transdermal and topical drug delivery with minimal tissue damage has been an area of vigorous research for years. Our research team has initiated the development of an effective method for delivering drug particles across the skin (transdermal) for systemic circulation, and to localized (topical) areas. The device consists of a laser ablation based micro-particle acceleration system that can be integrated with endoscopic surgical techniques. We have successfully delivered 3μm size cobalt particles into gelatin models that represent soft tissue with remarkable penetration depth.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2014.10a
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• pp.208-213
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• 2014

공동주택의 천장구조는 바닥충격음을 변화시키는 영향요소중의 하나이다. 천장구조의 진동응답 특성이 바닥충격음에 영향을 주는 요소를 확인하기 위해 천장구조의 달대를 제거하여 콘크리트 슬래브의 진동이 천장구조에 전달되지 않는 무달대 천장구조를 개발하였다. 달대가 시공된 일반 천장구조와 대비하여 무달대 천장구조의 천장판 가속도와 바닥충격음 레벨을 비교하였다. 무달대 천장구조를 사용함으로서 콘크리트 슬래브의 진동이 천장구조에 전달되는 것을 절연되어 천장구조의 진동응답 증폭을 저감시킬 수 있었으며, 저주파 대역의 바닥 충격음 증폭 또한 저감시킬 수 있었다. 일반 천장구조는 100 Hz 이하에서 천장구조의 진동응답이 증폭되어 저주파 대역 바닥충격음이 증폭되었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.310-319
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• 2017

This paper introduces the method how to measure the thrust in impulse facility. In a Facility having such a short duration time of steady flow, there's no time to reach a steady state of the forces acting on model so that the test model vibrates until the end of the flow. The forces exerted on an engine exist with vibration so that the usual force balance can not be used. SWFB(Stress Wave Force Balance) technique is utilized in a shock tunnel to get the thrust. As an example, a model force balance has been calculated its strain against impulse force by using FEM(Finite Element Method). A transfer function between the impulse force and strain has been obtained by the way of de-convolution.

• Journal of the Society of Naval Architects of Korea
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• v.33 no.2
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• pp.75-84
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• 1996

The structural response of naval surface ships subjected to underwater shock loadings is a very important problem in viewpoint ship survivability. In practice, among others the case of noncontact underwater explosions is the only one shock loading considered in designing naval surface ships to resist underwater explosions. In orator to efficiently design naval surface ships and their equipment to resist such shock loadings it seems necessary to prepare theoretical analysis tools and/or empirical design criteria which can predict the three dimensional transmission of shock waves. This paper describes a simplified method to analyse shock responses for ship hull girder, which uses a loading function to approximate the shock loadings on ship structures due to noncontact underwater explosions. A couple of examples to apply this method are provided.

• Journal of the Korean Society of Propulsion Engineers
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• v.20 no.5
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• pp.19-30
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• 2016

We presented a hydrodynamic modeling necessary to accurately reproduce shock-induced detonation of pyrotechnic initiator. The methodology for such numerical prediction of shock propagation is quite straight forward if the models are properly implemented and solved in a well-formulated shock physics code. A series of SSGT(Small Scale Gap Test) and detailed hydrodynamic simulation are conducted to quantify the shock sensitivity of an acceptor that contains 97.5% RDX. A TBI(Through Bulkhead Initiator) system, consisting of a train configuration of Donor(HNS+HMX) - Bulkhead(STS) - Acceptor(RDX), were investigated to further validate the interaction between energetic and non-reactive materials for predicting the detonating response for successful operation of such small pyro device.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2010.10a
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• pp.487-488
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• 2010

• Proceedings of the KSEEG Conference
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• 1999.04a
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• pp.217-222
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• 1999