This study investigates the microstructure and thermal shock properties of polycrystalline diamond compact (PDC) produced by the high-temperature, high-pressure (HPHT) process. The diamond used for the investigation features a 12~22 μm- and 8~16 μm-sized main particles, and 1~2 μm-sized filler particles. The filler particle ratio is adjusted up to 5~31% to produce a mixed particle, and then the tap density is measured. The measurement finds that as the filler particle ratio increases, the tap density value continuously increases, but at 23% or greater, it reduces by a small margin. The mixed particle described above undergoes an HPHT sintering process. Observation of PDC microstructures reveals that the filler particle ratio with high tap density value increases direct bonding among diamond particles, Co distribution becomes even, and the Co and W fraction also decreases. The produced PDC undergoes thermal shock tests with two temperature conditions of 820 and 830, and the results reveals that PDC with smaller filler particle ratio and low tap density value easily produces cracks, while PDC with high tap density value that contributes in increased direct bonding along with the higher diamond content results in improved thermal shock properties.

In this study, we performed non-elastic dynamic analyses using LS-DYNA for plate structures made of laminated composite materials. It was used mat_59_composite_failure_shell_model providing from LS-DYNA as material model of composite material The material which is applied in the analysis as CFRP and GFRP, were compared by performing the dynamic analysis in accordance with various layup sequences. Numerical results show structural resistance against impact loading for different materials. In addition, The significance of the layup sequence in analyzing composite structures under impact loading is enunciated in this paper

The honeycomb aluminum foam of the porous metal has the merit of the impact absorption, the soundproof, the heat conductivity, the light weight. Aluminum 6061-T6 is used at the materials for the automobile, the ship, the machine and various structures. In this study, the sandwich combined with the honeycomb aluminum foam and aluminum 6061-T6 is simulated with the impact. Two kinds of models made by use of CATIA program with 3 kinds of impact energies are analyzed by ANSYS program. As the simulation result, the maximum deformations at the cases of 1 and 2 are shown as 4.8205mm and 11.909mm respectively. And the maximum equivalent stresses at the cases of 1 and 2 are shown as 274.45MPa and 265.6MPa respectively. As the simulation result at case 1 approaches the experimental result, all simulation results can be verified in order to apply into analyzing the impact properties of the honeycomb aluminum foam sandwiches. In cases of three kinds of impact energies, the striker is not shown to penetrate the upper face sheets of case 1. At the impact energy of 100 J, the striker is not shown to penetrate the upper face sheets of case 2. At the impact energies of 200 J and 300 J, the striker is shown to penetrate the upper face sheets of case 2. It is thought to predict and improve the structural safety the composite material combined with the aluminium foam by using this study result.

구형 충격을 받는 필름 코팅된 유리 시스템의 거동을 개발한 유한 요소 프로그램에 의하여 연 구하고자 한다. 충격 거동을 예측하기 위하여 Sun의 higher order beam theory와 Kurapati의 generalized power law와 연계한 새롭고 효과적인 동적 유한 요소법을 제안한다. 필름 코팅된 유리 시 스템과 모놀리식 유리에 대하여 접촉력, 변형량, 운동에너지, 속도 및 응력 등을 계산한 후 결과를 비교 검토하여 코팅 시스템의 필름이 충격 손상을 방지하고 충격 저항이 우수하다는 것을 정성적 및 정량적으로 규명하였다.

LNG 방열 시스템의 선형 동적해석 모델을 사용하여 슬로싱 충격 압력을 구조해석에 적용 시 사용되는 이상화된 삼각파 압력에 대해서 검토하였다. 삼각파 압력의 최대값, 지속시간, 비대칭성의 충격파에 대한 구조 안전성 평가를 위해서 멤브레인 구조의 허용기준과 슬로싱 압력에 관련된 간략화된 파괴압력에 대해 검토하고, 슬로싱 충격 압력의 지속시간과 비대칭성으로 특징 지워진 이상화된 삼각파 형상의 압력을 고려한 일련의 선형 동적해석을 수행하여 설계기준으로 사용할 파괴압력을 도출하였다. 본 논문에서 제시한 방법을 통해서 방열시스템 구조 요소의 안전성을 평가하기 위한 파괴 압력을 선정할 수 있고 모형실험을 통한 슬로싱 압력과의 비교를 통하여 방열시스템의 구조안전성을 평가할 수 있을 것이라 판단된다. 또한 해석결과를 통해 방열시스템에서의 최대 응력은 매우 짧은 순간의 충격하중 하에서는 압력의 비대칭성 보다는 하중 지속시간에 많은 영향을 받고 있음을 검토하였다.

Micro structure observation for low carbon steel base material and heat treatment(annealing), performing a tensile test and impact test, the specimen after the impact test is intended to evaluate the crack propagation characteristics by performing a fractal dimension analysis. The tensile strength of the base materials were observed higher compared to the heat treated materials, impact absorbed energy of heat treated materials was a higher than base materials. Impact Test and fractal dimension of the side of the test specimen was shown significantly more test temperature increases, heat treated material was higher than the base material

Thermal shock resistance property has recently been considered to be one of the most important basic properties, in the same way that the transverse-rupture property is important for sintered hard materials such as ceramics, cemented carbides, and cermets. Attempts were made to evaluate the thermal shock resistance property of 10 vol% TaC added Ti(C,N)-Ni cermets using the infrared radiation heating method. The method uses a thin circular disk that is heated by infrared rays in the central area with a constant heat flux. The technique makes it possible to evaluate the thermal shock strength (Tss) and thermal shock fracture toughness (Tsf) directly from the electric powder charge and the time of fracture, despite the fact that Tss and Tsf consist of the thermal properties of the material tested. Tsf can be measured for a specimen with an edge notch, while Tss cannot be measured for specimens without such a notch. It was thought, however, that Tsf might depend on the radius of curvature of the edge notch. Using the Tsf data, Tss was calculated using a consideration of the stress concentration. The thermal shock resistance property of 10 vol% TaC added Ti(C,N)-Ni cermet increased with increases in the content of nitrogen and Ni. As a result, it was considered that Tss could be applied to an evaluation of the thermal shock resistance of cermets.

최근 급격히 변하는 기후 및 다양한 영향으로 인한 도로의 파손이 증가하는 추세를 보이고 있다. 그 중 포장의 성분 에 따른 강도의 문제로 파손이 발생되기도 하는데, 강도를 측정하는데 있어 아스팔트 혼합물은 탄성과 점성의 성질을 동시에 나타내기 때문에 온도 및 하중재하속도, 간격을 매우 중요한 인자로 고려한다. 이러한 인자들을 만족시키기 위 하여 국내에서는 고가의 장비에 의존하고 있는 실정이다. 이러한 점에 대해 본 연구에서는 상대적으로 저렴한 동시에 빠르게 동탄성계수를 도출해 내기 위해서 IRT시험을 도입하였다. 또한 IRT 시험법 평가를 위하여 공신력을 가지고 있 는 MTS 장비의 결과와 비교하고자 한다. MTS 810시스템을 사용하여 동탄성계수를 측정하는데 있어 실험조건으로 하중주기 주파수는 0.0001, 0.0005, 0.001, 0.005, 0.01, 0.02KHz로 설정하였으며, 실험온도는 5, 20, 40, 54℃로 설정하여 수행하였다. 일축압축/인장시험 수행에 서는 공시체에 120°간격으로 85mm 변형측정자기센서(Linear Variable Differential Transformer, LVDT) 4기를 설치 하여 수직변형을 측정하는 방식으로 수행되었다. IRT 시험에서는 아래 Figure 2와 같이 공시체를 고정시킨 후 한쪽 면을 쇠구슬로 충격을 가한다. 이때 공시체 양 측면에 가속도계를 설치하여, 쇠구슬로 인해 발생하는 외력에 대한 신호를 계측 한다. 이 아날로그 신호는 펄스장비를 통하여 디지털 신호화 되어지며, 이때 신호의 전파속도가 상당히 빠르기 때문에 신 호처리와 공진주파수를 찾기 위하여 시간에 대한 디지털신호를 주파수에 대한 Frequency Function으로 변환하는 과정을 수행한다.

This paper presents a method for the assesment of thermal and vibration fatigues in integral exhaust manifold/turbine housing system. Most of failures on turbine housing are observed by thermal cyclic loads. In order to predict thermal failures by finite element analysis, we considered the temperature-dependent inelastic materials and transient temperature histories based on the thermal shock test. The results showed that the plastic strains of localized critical regions such as valve seat coincided well with crack locations from an endurance test. But, some failures around neck areas of turbine housing could not predict from thermal stress analysis. These cracks were originated due to the vibration excitations near resonance frequencies within engine operating ranges. The stress results of neck areas, which divided by temperature dependent yield stresses, from harmonic analysis showd a good agreement with experimental results.

The improvement of car driving comfort is requested according to development of automobile manufacturing technology. Therefore, many experts have been studying automotive vibration of normally driving cars to improve automotive driving comfort. Vibration characteristics of a tire play an important role to judge a ride comfort ability and sound quality for a vehicle. A lots of study on the ride and the noise to reduce the vibration in the 20∼100Hz frequency range was being carried out for years. The tire impact due to the bump is the main factor of the vibration in the 20∼100Hz. This vibration is related to the harshness which perceive the displeasure or noise. In this study, we investigated the characteristics of the impact harshness due to the stiffness of the tire tread part according to change the tread compound.

The monolithic glass, without damage, under impact loading, is studied by the use of the coded finite element program. To predict the impact energy of monolithic glass like annealed glass and tempered glass, a finite element approach based on Sun's higher-order beam finite element and impact energy equation is proposed. For this purpose, the contact force-displacements, energy-displacement histories and velocity-acceleration histories etc. are calculated during all impact processes. And, also, by the calculations of the coded FEM program, the geometric parameter like thickness is investigated to determine their impact energy prediction of monolithic glass.

The monolithic glass, without damage, subjected to ballistic impact, is studied by the use of the coded finite element program. To analyze the impact response of monolithic glass like ordinary annealed glass and tempered glass, a finite element approach based on the Hertzian contact law and Sun's higher-order beam finite element is proposed. For verifying effectiveness of this finite element program, the contact force history is analyzed in conjunction with the loading and unloading processes. And, also, the time history of the impact responses such as the strain and stress according to the thickness changes due to transverse impact at the center are calculated

In this study, nanocrystalline Cu-Ni bulk materials with various compositions were cold compacted by a shock compaction method using a single-stage gas gun system. Since the oxide layers on powder surface disturbs bonding between powder particles during the shock compaction process, each nanopowder was hydrogen-reduced to remove the oxide layers. X-ray peak analysis shows that hydrogen reduction successfully removed the oxide layers from the nano powders. For the shock compaction process, mixed powder samples with various compositions were prepared using a roller mixer. After the shock compaction process, the density of specimens increased up to 95% of the relative density. Longitudinal cross-sections of the shock compacted specimen demonstrates that a boundary between two powders are clearly distinguished and agglomerated powder particles remained in the compacted bulk. Internal crack tended to decrease with an increase in volumetric ratio of nano Cu powders in compacted bulk, showing that nano Cu powders has a higher coherency than nano Ni powders. On the other hand, hardness results are dominated by volume fraction of the nano Ni powder. The crystalline size of the shock compacted bulk materials was greatly reduced from the initial powder crystalline size since the shock wave severely deformed the powders.

충격 및 폭발하중으로 인한 위험으로부터 구조물의 안정성을 확보하기 위한 필요성의 증대에 따라 고율변형을 받는 콘크리트의 거동은 중요한 연구주제가 되었다. 콘크리트의 고율변형 거동은 정적인 상태와는 다른 독특한 거동을 보이기 때문에 다양한 고율변형모델들이 제안되어 고율변형 상태를 수치해석하는데 사용되고 있다. 이러한 수치해석 과정에서 발생하는 문제가 요소의 크기에 따라 수치해석결과가 크게 변하는 요소의존성 문제이다. 본 논문에서는 파괴에너지이론에 기초하여 요소의존성을 최소화할 수 있는 기준식을 제안하고 HJC(Holmquist Johnson Cook)모델을 이용한 관통수치해석을 통해 기준식을 검증하였다. 그 결과 기준식을 통해 산정된 파괴변형률을 수치해석상에 적용해줌으로써 해석결과의 요소의존성이 감소하였고 해의 정확성 또한 향상되는 것을 파악할 수 있었다.

PURPOSES: The dynamic modulus can be determined by applying the various theories from the Impact Resonance Testing(IRT) Method. The objective of this paper is to determine the best theory to produce the dynamic modulus that has the lowest error as the dynamic modulus data obtained from these theories(Complex Wave equation Resonance Method related to either the transmissibility loss or not, Dynamic Stiffness Resonance Method) compared to the results for dynamic modulus determined by using the Universal Testing Machine. The ultimate object is to develop the predictive model for the dynamic modulus of a Linear Visco-Elastic specimen by using the Complex Wave equation Resonance Method(CWRM) came up for an existing study(S. O. Oyadiji; 1985) and the Optimization. METHODS: At the destructive test which uses the Universal Testing Machine, the dynamic modulus results along with the frequency can be used for determining the sigmoidal master curve function related to the reduced frequency by applying Time-Temperature Superposition Principle. RESULTS: The constant to be solved from Eq. (11) is a value of 14.13. The reduced dynamic modulus obtained from the IRT considering the loss factor related to the impact transmissibility has RMSE of 367.7MPa, MPE of 3.7%. When the predictive dynamic modulus model was applied to determine the master curve, the predictive model has RMSE of 583.5MPa, MPE of 3.5% compared to the destructive test results for the dynamic modulus. CONCLUSIONS: Because we considered that the results obtained from the destructive test had the most highest source credibility in this study, the dynamic modulus data obtained respectively from DSRM, CWRM were compared to the results obtained from the destructive test by using th IRT. At the result, the reduced dynamic modulus derived from DSRM has the most lowest error.

PURPOSES: The dynamic modulus for a specimen can be determined by using either the non-destructed or destructed testing method. The Impact Resonance Testing (IRT) is the one of the non-destructed testing methods. The MTS has proved the source credibility and has the disadvantages which indicate the expensive equipment to operate and need a lot of manpower to manufacture the specimens because of the low repeatability with an experiment. To overcome these shortcomings from MTS, the objective of this paper is to compare the dynamic modulus obtained from IRT with MTS result and prove the source credibility. METHODS: The dynamic modulus obtained from IRT could be determined by using the Resonance Frequency (RF) from the Frequency Response Function (FRF) that derived from the Fourier Transform based on the Frequency Analysis of the Digital Signal Processing (DSP)(S. O. Oyadigi; 1985). The RF values are verified from the Coherence Function (CF). To estimate the error, the Root Mean Squared Error (RMSE) method could be used. RESULTS : The dynamic modulus data obtained from IRT have the maximum error of 8%, and RMSE of 2,000MPa compared to the dynamic modulus measured by the Dynamic Modulus Testing (DMT) of MTS testing machine.. CONCLUSIONS: The IRT testing method needs the prediction model of the dynamic modulus for a Linear Visco-Elastic (LVE) specimen to improve the suitability.

In this study, carbon fiber reinforced plastic and aluminum foam used in impact absorber are assembled and modelled. These models are investigated by impact simulation and verified by experimental data. Impact energies of 30 J, 60 J and 100 J are applied on these specimens by striker. For example the experiment for impact energy of 30 J is done and verified by referring to analysis result. As the structural safeties of these assembled composite materials can be anticipated through this study result, these simulation analysis results can be applied into real field.

위석은 소화된 음식물이 축적되어 구성된 위장내 덩어리 이다. 담도위석은 매우 드문 형태의 위석으로 주로 담낭절 제술의 과거력을 가진 환자에서 발생하는데 유두부 괄약근 기능 소실이 원인이 되어 십이지장에서 담도내로 소화되지 않은 음식물을 비롯한 이물질이 역류하여 발생하는 것으로 생각된다. 이러한 담도위석의 치료로 내시경적 역행성 췌담관 조영술을 통한 유두부로의 제거를 시도해볼 수 있으나 본 증례처럼 거대크기의 담도위석은 유두부를 통한 제거가 불가능하고 수술적 치료가 필요한 경우가 많다. 체외 충격 파 쇄석술은 신장결석이나 요로결석의 파편화에 이용되는 기술로 담도결석에서도 드물게 이용되는데, 본 증례는 개복 담낭절제술 및 총담도-십이지장 문합술의 과거력을 가진 담도위석 환자에서 커다란 크기로 인하여 두차례 체외 충격파 쇄석술을 통하여 분쇄후 내시경 역행성 췌담관 조영 술로 제거한 흔치 않은 증례이며 거대담도위석의 안전하고 간단한 치료대안으로 생각된다.

Bulk nanostructured copper was fabricated by a shock compaction method using the planar shock wavegenerated by a single gas gun system. Nano sized powders, average diameter of 100 nm, were compacted into the cap-sule and target die, which were designed to eliminate the effect of undesired shock wave, and then impacted with analuminum alloy target at 400 m/s. Microstructure and mechanical properties of the shock compact specimen were ana-lyzed using an optical microscope (OM), scanning electron microscope (SEM), and micro indentation. Hardness resultsshowed low values (approximately 45~80 Hv) similar or slightly higher than those of conventional coarse grained com-mercial purity copper. This result indicates the poor quality of bonding between particles. Images from OM and SEMalso confirmed that no strong bonding was achieved between them due to the insufficient energy and surface oxygenlayer of the powders.

항공기 연료셀은 추락 상황에서 승무원의 생존성과 직결되는 중요 구성품으로 회전익 항공기에 적용되고 있는 내충격성 연료셀은 추락시 승무원의 생존성 향상에 큰 역할을 하고 있다. 미육군은 항공기가 처할수 있는 다양한 상황에서 연료셀이제 기능을 발휘할 수 있도록 1960년대 초부터 MIL-DTL-27422 이라는 연료셀 개발규격을 제정하여 현재까지 적용해 오고있다. 해당 개발규격에 규정된 시험 중에서 충돌충격시험은 연료셀의 내충격 성능을 검증하는 시험으로써, 해당 시험을 통과하는 연료셀은 생존가능 충돌환경에서 화재가 발생하지 않아 승무원의 생존성이 대폭 향상될 수 있음을 의미한다. 그러나 충돌충격시험은 작용하는 하중 수준이 너무 높기 때문에 실패 위험성이 가장 큰 시험이기도 하다. 연료셀이 해당 시험을 통과하지 못하는 경우에는 재시험을 위한 비용과 준비기간이 상당히 소요되어 항공기 개발일정에 심각한 지장을 초래할 가능성도 높다. 따라서, 연료셀 설계 초기부터 내충격성능 만족여부에 대한 예측을 위해 충돌충격시험의 수치해석을 통한 실물시험에서의 실패 가능성을 최소화해야 한다는 필요성이 제기되어 왔다. 본 연구에서는 충돌모사 프로그램인 LS-DYNA에서 지원하는 유체-구조 연성해석 방법인 SPH 방법을 사용하여 연료셀 충돌충격시험 수치 모사를 수행하였다. 수치해석 조건으로 MIL-DTL-27422에서 요구하는 시험조건을 고려하였고, 실물 연료셀의 시편시험을 통해 확보한 물성데이타를 해석에 반영하였다. 그 결과로 연료셀 자체의 응력수준을 평가하고 취약부위에 대한 고찰을 수행하였다.