• Composites Research
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• 제29권2호
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• pp.60-65
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• 2016

In this paper, finite element analysis and real time monitoring experimental work using FBG sensor were carried out for analyzing structural integrity of a Type IV hydrogen pressure vessel under impact loading condition. By using finite element analysis with the ply based modeling technique, sensor insertion points and pressure condition were suggested. Tensile test with an angle ply specimen was conducted for getting the reliability of FBG sensor insertion method. After fabricating the vessel, total five times pressurization fatigue tests were conducted (Non-impact pressurization: 1, After impact pressurization: 4). Experimental results revealed that filling cycle time was gradually increased and filling gradient was decreased when the vessel experienced impact.

• Transactions of the Korean Society of Mechanical Engineers B
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• 제39권5호
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• pp.385-390
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• 2015

The flow characteristics in micro shock tube are investigated experimentally. Studies were carried out using a stainless steel micro shock tube. Shock and expansion wave was measured using 8 pressure sensors. The initial pressure ratio was varied from 4.3 to 30.5, and the diameter of tube was also changed from 3mm to 6mm. Diaphragm conditions were varied using two types of diaphragms. The results obtained show that the shock strength in the tube becomes stronger for an increase in the initial pressure ratio and diameter of tube. For the thinner diaphragm, the highest shock strength was found among varied diaphragm condition. Shock attenuation was highly influenced by the diameter of tube.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 한국추진공학회 1998년도 제11회 학술강연회논문집
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• pp.10-10
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• 1998

천음속 익형에서 발생하는 응축충격파와 경계층의 간섭을 피동제어 하여 항력감소에 대한 연구를 2.5$\times$7$\textrm{cm}^2$ 천음속 풍동에서 수행하였다. 익형표면에 설치한 정압공으로 정압을, 익형후방에 설치한 8개의 Pitot probe로 전압을 동시에 측정하여 충격파를 통한 에너지의 손실과 항력의 변화를 계산하였고, 또한 유동장과 충격파의 형상을 가시화하기 위해 슈리렌 가시화 시스템을 사용하였다. 실험은 NACA 0012 익형에서 기공률 변화에 따른 피동제어의 항력감소 초과를 조사한 다음 NACA 64-018 익형에서는 기공률과 공동의 크기의 변화가 미치는 효과를 연구하였다. 피동제어의 개념은 충격파가 발생하는 하부벽을 다공벽으로 만들고 그 아래를 공동으로 만들면 충격파 후방의 상대적으로 높은 압력이 기류의 일부를 공동으로 자연스럽게 유입시키고 다시 공동에서 낮은 압력의 충격파 상류로 유출시키는 것이다.

• Journal of Korean Society of Steel Construction
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• 제28권4호
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• pp.271-280
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• 2016

The need to accurate quantification of blast pressure loading in the near field is important because the focus of security design of critical infrastructure, buildings and bridges is for near-field detonations. Incident and reflected pressures for near-field detonations are very difficult to be measured by commercially available pressure transducers due to the high pressure and temperature, which requires a verified and validated computational fluid dynamics code to reasonably predict the near-field pressures and impulses. This paper presents numerical studies to verify and validate a CFD code for calculations of incident and reflected overpressures and impulses. The near field is emphasized and recommendations for mesh sizes to optimally simulate the near-field detonation are provided.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 한국추진공학회 2008년도 제30회 춘계학술대회논문집
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• pp.295-298
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• 2008

In this paper, prototype dynamic modeling scheme to control ramjet propulsion systems were proposed. From the physical understandings of engine system, a typical 2nd-order system model was applied to simulate the dynamic characteristics of fuel supply system. The shock location varience in diffuser to chamber pressure fluctuation is calculated so that the out of phase between two signals was observed.

• Journal of the Korean Society of Propulsion Engineers
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• 제16권5호
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• pp.74-80
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• 2012

Past few years have seen the growing importance of micro shock tubes in various engineering applications like micro combution, micro propulsion, particle delivery systems. But in order to efficiently apply Micro Shock Tube to such areas require the detailed knowledge of shock characteristics and flow field inside a micro shock tube. Due to many factors such as boundary layer, low Reynolds number and high Knudsen number shock propagation inside micro shock tubes will be quite different from that of the well established macro shock tubes. In the present study, experimental studies were carried out on micro shock tubes of two diameters to investigate flow characteristics and shock propagation. Pressure values were measured at different locations inside the driven section. From the experimental values other parameters like shock velocity, shock strength were found and shock wave diagram was constructed.

• Journal of Ocean Engineering and Technology
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• 제24권6호
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• pp.30-33
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• 2010

This study presents the effect of filling ratio on sloshing impact pressure. The experiment was done with three filling ratios of 20%, 70%, and 95% of the tank height. The input of the motion was regular excitation. The total number of sensors in use were 53. They were installed on tank top and tank wall. The maximum pressures and the average of one third highest impact pressures for the whole pressure sensors were investigated. The result shows clearly the location of sensors which are exposed to the high impact pressures for different filling ratios. The characteristics of the impact patterns for three filling ratios were also examined.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• 제43권6호
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• pp.479-487
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• 2015

In a reflected shock tunnel, stagnation conditions of a nozzle are determined by the flow behind a reflected shock. When calculating the flow behind the reflected shock, unlike a shock tube, the flow leakage through the nozzle is to be considered. The analytical studies were done to find out the characteristics of the stagnation conditions of the nozzle with various nozzle throat size. Experiments and numerical simulations were also carried out for further understanding of the flow leakage effects. It was found that the nozzle stagnation pressure was diminished by the increase of the size of the nozzle throat. It was also found that the steady pressure in the stagnation were maintained well at the area ratio of the driven tube to the nozzle throat is 4.5.

• Proceedings of the Korea Water Resources Association Conference
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• 한국수자원학회 2018년도 학술발표회
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• pp.290-290
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• 2018

본 연구에서는 수충격으로 발생할 수 있는 실제 상수도관망의 피해율을 신뢰성해석을 통해 정량적으로 비교분석하였다. 이를 위해서 먼저 실제 상수관망에 대한 수충격해석을 수행하였는데 기존의 가압장 운영조건을 적용하였고 가압장의 선택운영조건을 변경하여 수충격해석을 수행하였다. 이 결과물을 토대로 신뢰성해석을 수행하였고 두 조건에 대하여 정량적인 파괴확률을 산정할 수 있었다. 본 연구에서 사용된 실제 상수관망은 가압장의 운영조건으로 24시간 75m 수두를 유지하고 있으며 관말단부의 수용가에 충분한 유량이 전달되고 있다. 가압장의 고압유지는 관말부에는 적정할 수 있으나 상수도관망에서 누수와 시설물에 대한 많은 피해를 유발할 수 있다. 따라서 본 연구에서는 가압장의 펌프압력수두를 75m와 65m로 선택적 운영을 가정하였다. 이로 인한 관말부의 압력이 수도압력으로 충분한 15m를 계속 유지하는 것을 확인하였으며 수돗물 사용량이 적은 야간에는 가압장의 수두를 낮추는 방법으로 선택적 운영조건을 사용하였다. 기존 가압장의 운영조건과 선택적 운영조건을 사용하여 수충격해석을 수행하였고 신뢰성 해석모형을 사용하여 파괴확률을 정량적으로 산정할 수 있었다. 가압장의 운영조건을 최적화하여 효율은 증대하고 피해율을 저감할 수 있는 방법을 찾을 수 있었다, 이를 위해서 가압장의 인버터 설치는 물론이고 펌프의 최적운영을 위한 프로그램을 장착하여 가압장을 운영한다면 보다 경제적인 운영이 될 수 있을 뿐만 아니라 실제 상수관망에서 발생할 수 있는 여러 가지 피해를 최소화할 수 있을 것으로 판단된다.

• Journal of the Korea Academia-Industrial cooperation Society
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• 제11권8호
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• pp.2741-2749
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• 2010

This paper presents the impact damage behavior of filament wound composite vessels and the effect of surface protective materials on their impact resistance. Using an instrumented impact testing machine, a series of impact tests was performed on the base panels and the protected panels (panels with surface protective materials of rubber, kevlar/epoxy or glass/epoxy laminates) that were cut from the full scale vessel. And the impact damage parameters were used to identify the effect of protective materials on the damage resistance of composite vessels. Damage resistance of the composite vessels was considerably affected by the protective materials regardless of the shape of the indenters. Among the protective materials, glass/epoxy laminates was the most effective mean for improving the damage resistance of composite vessels.