• Proceedings of the Korean Society of Computer Information Conference
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• 2022.07a
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• pp.315-316
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• 2022

본 논문은 스마트 인솔의 압력 데이터를 이용하는 컨볼루션 신경망 모델에 해석가능한 인공지능 방법인 Grad-CAM을 적용하는 방법을 제안한다. 학습된 각 모델에 Grad-CAM을 적용하여 모델에서 중요한 역할을 하는 압력센서와 중요하지 않은 압력센서를 알아내는 방법을 제안하고 데이터마다 학습을 진행하고 학습된 모델을 통해 실제로 중요한 압력센서와 그렇지 않은 압력센서에 대해서 알아본다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.7
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• pp.531-538
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• 2017

A flush air data sensing system, which can predict flight speed, angle of attack, and angle of sideslip of the aircraft is designed and manufactured for a small UAV. Two kinds of flush pressure ports, four ports and five ports, are tapped at the same section of fuselage nose-cone. Calibration pressure data at flush ports are obtained through computations for the total aircraft by using Fluent code. Angle of attack, angle of sideslip, total pressure, and static pressure are represented with 4th-order polynomial function and calibration coefficient matrix is obtained using least square method with calibration pressure data. Flight test showed that flight speed, angle of attack, and sideslip angle predicted by four flush ports and five flush ports compared well with those by five-hole probe installed for data comparison. Especially four flush ports revealed nearly same results as those by five flush ports.

• Journal of the Korean Society of Marine Environment & Safety
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• v.18 no.4
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• pp.371-377
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• 2012

This paper presents an experimental investigation to figure out slamming impact pressure and flow characteristics of a rectangular Marine structure($800{\times}250{\times}50mm^3$) in free fall. The flow field has been obtained by 2-frame grey level cross correlation PIV(Particle Image Velocimetry) method, the impact pressure of the free fall model by a pressure acquisition system(Dewatron). The angles between a model and the free surface are adapted $10^{\circ}$ and $20^{\circ}$ respectively. Velocity field of water exit has higher better than water entry. The highest point, P2 of impact pressure under the bottom of the model has been appeared about 6 % higher values at 20 degrees than 10 degrees.

• Journal of Biomedical Engineering Research
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• v.19 no.4
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• pp.423-429
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• 1998

Human pharynx is unique, acting as a complex interchange between the oral cavity and esophagus, and between the nasal cavity and lungs. It is actively involved in the transport of food and liquid, producing the forces that guide that bolus into the upper esophagus and away from the adjacent larynx and lungs. This study intended to develop a biomechanical model of the human pharynx, utilizing Finite Element Method(FEM). Within each model changes in cross sectional intralumenal area were calculated and compared with the area from the computer-generated FE model. Area matching allowed estimation of intraluminal pressure gradients during swallow. The estimated pharyngeal pressure gradient varies from one region to another. The estimated pharyngeal pressure gradients showed different patterns for upper four levels and lower four levels. The contraction velocity for upper four levels is much higher than lower four levels. The higher contraction velocities and pressure gradients in the upper levels are consistent with the bolus velocities required for efficient swallow.

• Explosives and Blasting
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• v.37 no.4
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• pp.10-16
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• 2019

Information on overpressure, positive phase duration, and impulse are required to assess the effects of shock waves or pressure waves on the structure. In this study, the overpressure and positive phase duration were determined by applying the Multi-Energy Method, which is found to be effective in analyzing the explosion of vapor clouds. Based on the total heat of combustion estimated in the cyclohexane vapor cloud explosion in the Nypro Ltd(UK), overpressure and positive phase duration at the distance of 40, 80, 120, 160, 200, 240, 280, 320, 360(m) from the source of explosion were evaluated. Overpressure was shown to decrease exponentially and positive phase duration increased almost linearly with distance. A probit function was used to assess the probability of damages for the structures at each distance using the overpressure and impact obtained at the above mentioned distances. The Analyses of probability of damages have shown that there is a high probability of collapse at distances within 120m, major damage to structures within 240m, and minor damage and breakage of window panes of structures occur over the entire distances.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.20 no.6
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• pp.402-409
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• 2019

Patients with dementia or elderly patients who can not move at all by themselves are at a high risk of falls and bedsore due to lack of caregivers. In this paper, to solve this problem, we propose an algorithm to determine the patient's lying postures by discriminating the main body parts such as head, shoulders, and hips based on the pressure intensity sensed at regular intervals. A smart mat with a lattice structure in which a pressure sensor is arranged so that the body part can be discriminated irrespective of the physical characteristics has been implemented. It consists of two modules of $7{\times}7$ array size. Each module consists of 49 FSR-406 sensors and independently senses pressure. For each module, the body part corresponding to the upper body or the lower body is sequentially discriminated by using a pressure distribution such as a cumulative pressure sum using a filter. The proposed algorithm can identify five lying positions by examining the inclusion relationship between body parts belonging to layer-1 such as head, shoulder, and hip area.

• Composites Research
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• v.19 no.3
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• pp.7-14
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• 2006

In this paper, an integrated probabilistic strength analysis was conducted to predict the reliability of a composite pressure vessel under inner pressure loading condition. As a probabilistic strength analysis, the probabilistic progressive failure model consisting of progressive failure model and Monte Carlo simulation was incorporated with a commercial FEA code, ABAQUS Standard, to perform the probabilistic failure analysis of composite structure which has a complex shape and boundary conditions. As design random variables, the laminar strengths of each direction were considered. Finally, from probabilistic strength analysis, the scattering of burst pressure could be explained and the reliability of composite pressure vessel could be obtained for each component. In case of composite structures in mass production, the effects of uncertainties in material and manufacturing on the performance of composite structures would apparently become larger. So, the probabilistic strength analysis is essential for the structural design of composite structures in mass production.

• The Journal of Korea Institute of Information, Electronics, and Communication Technology
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• v.15 no.5
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• pp.349-359
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• 2022

The aim of this study is to analyze the dynamic characteristics of proportional control valves according to various working conditions as a basic study for developing proportional control valves for auto-steering tractors. The dynamic characteristics of proportional valves were measured using hydraulic characteristics measurement system, and the power was analyzed using measured flow rate and pressure data. As the experimental conditions, the tractor engine speed and steering angle was selected as the main variables, and the experiment was performed on urethane road conditions. As a result, it was found that the flow rate, pressure, and power of the proportional control valve increased as the tractor engine speed and steering angle increased. In particular, as the steering angle increased at the same engine speed, the flow rate, pressure, and power tended to increase by up to 190%, 172%, and 273%, respectively. Similarly, as the engine speed increased at the same steering angle, the flow rate, pressure, and power tended to increase up to 161%, 122%, and 168%, respectively. Therefore, it can be seen that the steering angle has a higher influence on the dynamic characteristics of the proportional control valve than the engine speed.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.10
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• pp.7-15
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• 2006

The effects of strake incidence-angle on the vortex characteristics and the wing-surface pressure distribution for a double-delta wing with strake were investigated experimentally. The strake incidence-angle of negative sign(strake is pitched down from the main-wing upper-surface) increased the suction pressure of the wing-upper surface, which was the same effect of increase of angle of attack. This change of the suction pressure was caused by the closer movement of the vortex cores to the wing upper surface rather than the increase of the vortex strength.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.08a
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• pp.163.1-163.1
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• 2013

플라즈마 시뮬레이션을 수행하기 전에 현 컴퓨터의 계산 능력범위 내에서 물리적으로 타당하게 설명할 수 있는 수치 해석 방법을 먼저 정한다. 예를 들면, 가스 반응이 많고 각 가스 반응 중에 중요가스 반응을 빠르고 선택적으로 선별하고자 할 때, 혹은 외부 입력 변화에 따른 플라즈마 종의 온도 또는 밀도를 대략적으로 파악하고자 할 때는 공간적인 분포를 고려하지 않는 0차원 global 모델링을 이용한다. 압력이 높고 충돌이 빈번한 경우에는 플라즈마를 유체적인 관점에서 기술이 가능하므로, 볼츠만 방정식에서 속도에 관한 0차, 1차, 2차 모멘텀을 이용하여 유도된 유체 방정식을 이용한다. 반대로 압력이 낮고 충돌이 거의 없는 경우에는 플라즈마 입자를 개별적으로 추적하는 입자 전산 모사 방법을 이용한다. 지금까지는 앞에서 언급한 예와 같이, 개별 플라즈마 상태에 맞는 시뮬레이션 코드를 각각 만들어야 했고, 각 코드를 개별적으로 유지 보수해야 했다. 하지만, 개별적으로 코드를 유지 보수를 해야 할 경우에는, 동일한 기능을 하는 함수를 반복적으로 각 코드에 입력해야 하는 불편함이 따르고, 각 수치해석 방법의 장점을 모은 하이브리드 방법과 같은 전사모사를 개발할 때 각 기능을 통합해야 하는 어려움이 따른다. 또한 지금까지 개발된 대부분의 플라즈마 코드는 외부 입력에 대해 유연하지 못한 대처로 새로운 가스 반응을 추가하거나 새로운 수치해석 방법을 추가할 경우에는 코드를 전체적으로 수정해야 하는 어려움이 있었다. 따라서 코드를 통합적으로 관리할 수 있고, 외부 입력에 대해 유연하게 대처할 수 있는 시뮬레이터가 필요했다. 여기에서는 객체 지향 언어인 C++ 언어를 이용하여, 사용자 입력에 대해 유연하게 대처할 수 있고, 복잡한 화학 반응을 특정 수치 해석 방법에 상관없이 통합적으로 관리할 수 있는 코드를 개발하였다.