• 한국재료학회지
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• 제26권7호
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• pp.370-375
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• 2016

Tensile tests and creep tests were carried out at high temperatures on an Al-$Al_4C_3$ alloy prepared by mechanical alloying technique. The material contains about 2.0% carbon and 0.9% oxygen in mass percent, and the volume fractions of $Al_4C_3$ and $Al_2O_3$ particles are estimated at 7.4 and 1.4%, respectively, from the chemical composition. Minimum creep rate decreased steeply near two critical stresses, ${\sigma}_{cl}$ (the lower critical stress) and ${\sigma}_{cu}$ (the upper critical stress), with decreasing applied stress at temperatures below 723 K. Instantaneous plastic strain was observed in creep tests above a critical stress, ${\sigma}_{ci}$, at each test temperature. ${\sigma}_{cu}$ and ${\sigma}_{ci}$ were fairly close to the 0.2% proof stress obtained by tensile tests at each test temperature. It is thought that ${\sigma}_{cl}$ and ${\sigma}_{cu}$ correspond to the microscopic yield stress and the macroscopic yield stress, respectively. The lower critical stress corresponds to the local yield stress needed for dislocations to move in the soft region within subgrains. The creep strain in the low stress range below 723 K arises mainly from the local deformation of the soft region. The upper critical stress is equivalent to the macroscopic yield stress necessary for dislocations within subgrains or in subboundaries; this stress can extensively move beyond subboundaries under a stress above the critical point to yield a macroscopic deformation. At higher temperatures above 773 K, the influence of the diffusional creep increases and the stress exponent of the creep rate decreases.

• 한국농공학회지
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• 제20권4호
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• pp.4805-4811
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• 1978

This paper deals with the correlations between the results of the physical property tests and the mechanical property tests for estimating the mechanical indexes by the physical property test results. The soil samples were taken at changweon area, Gyeon-gsangnam-do, where the structures would be placed on the alluvial clay foundation. The outcomes of the study are as follows: 1. Judging from casagrande's plasticity chart, it is considered that the almost all soil samples belong to inorganic silty clay with medium plasticity (clay 14∼62%, silt 36∼73%, sand 1∼29%). The specific gravities are between 2.61 and 2.72, the wet unit weights 1.53g/㎤ and 1.93g/㎤, the liquid limits 28% and 51%, the plastic limits 15% and 31%, the plastic indexes 7% and 27%, the natural moisture contents 33% and 64%. 2. The unconfined compression strengths are between 0.07kg/$\textrm{cm}^2$ and 0.77kg/$\textrm{cm}^2$, the cohesions 0.04kg/$\textrm{cm}^2$ and 0.37kg/$\textrm{cm}^2$, the internal friction angles 0$^{\circ}$ and 9$^{\circ}$. 3. The consolidation tests show that the initial void ratios are between 0.68 and 1.68, the precompression loads 0.27kg/$\textrm{cm}^2$ and 1.15kg/$\textrm{cm}^2$, the compression indexes 0.12 and 0.59. 4. The correlations between the results of the physical property tests and the mechanical property tests for the soil samples are presented as follows: rt=0.011 (203-wn), Cc=0.025 (LL-27.2), Cc=0.46 (e0-0.58), Cc=0.013 (wn-23.2), C=0.021+qu/2.08, qu=2.268rt-3.635

• 한국항공우주학회지
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• 제43권6호
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• pp.526-532
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• 2015

국내개발 헬기인 수리온의 악기상 시 운용능력을 입증하고 결빙하 운용 제한 사항을 해제하기 위하여 결빙 감항인증이 요구되고 있다. 군용헬기인 수리온의 결빙 감항인증 절차는 유사 무기체계인 UH-60과 AH-64의 사례와 S/W 기술의 성숙도를 보았을 때, 전산해석${\rightarrow}$모의결빙형상 비행시험${\rightarrow}$인공 결빙 비행시험${\rightarrow}$자연 결빙 비행시험의 4가지 방법에 의한 단계화된 추진이 고려되고 있다. 수리온의 최적 비행시험 소티와 비행시간은 인공 결빙 비행시험 20~30소티 및 20~23시간과 자연 결빙 비행시험 20~30소티 및 20~22시간이 요구되며, 효율적인 결빙 감항인증 비행시험을 위해서는 LWC $0.5{\sim}1.0g/m^3$범위의 대기온도 조건은 인공 결빙 비행시험을 추진하고, LWC $0.5g/m^3$이하의 대기온도 조건에서는 자연 결빙 비행시험이 필요하다.

• 대한치과교정학회지
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• 제33권6호
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• pp.465-474
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• 2003

형상기억효과 및 초탄성 특성을 가진 니켈 타이타늄 와이어는 대단히 다양한 제품들이 출시되어 있어서, 보다 적절하면서도 경제적인 재료를 선택하고자 하는 임상가에게 어려움을 주고 있다. 이때, 교정 선재의 기계적 특성에 대한 실험적 연구는 임상가에게 유용한 정보를 제공해 줄 수 있다. 이 연구에서는 5군으로 나뉘어진 4종의 교정선재(stainless steel, multistranded, superelastic nickel titanium 그리고 themoactivated nickel titanium)에 대한 응력 -변형 실험을 통한 기계적 특성에 대한 비교를 시행하였다. 각 군의 교정선재에 대하여 일련의 여섯 가지 실험이 이루어졌다. 처음에는, 각 군에 대하여 선재가 파절될 때까지, 3차례의 실험이 이루어졌다. 그리고, 각 군에서 세 종류의 실험이 이루어졌는데, 표준하중에서 선재를 신장시켜서, 하중을 주었을 때와 하중을 제거하였을 때의 기계적 특성에 대한 신뢰할 만한 비교를 시행하였다. 각 군간의 차이를 알아보기 위하여 t-test를 시행하였다. 실험결과, 생리적인 치아이동을 위한 기계적 특성, 즉 강성, 탄성률, 힘의 발휘 특성 등을 고려해 볼 때, themoactivated nickel titanium, multistranded wire, stainless steel wire 순으로 바람직하였다. 초탄성은 superelastic nickel titanium에서 나타났다. 섭씨 37도에선 themoactivated nickel titanium의 형상기억효과가 나타났는데, 이것은 온도가 기계적 특성을 증진시키는데 중요하다는 것을 보여준다.

• 대한기계학회논문집A
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• 제31권10호
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• pp.1017-1024
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• 2007

This study performed a series of burst tests at ambient temperature using real-scale elbow specimen containing a local wall-thinning defect at it's intrados or extrados and evaluated failure pressure of locally wall-thinned elbows. In the experiment, a 90-degree 100A, Sch. 80 standard elbow was employed, and various wall-thinning geometries, such as length, depth, and circumferential angle, were considered. From the results of experiment, the dependences of failure pressure of wall-thinned elbows on the defect geometries and locations were investigated. In addition, the reliability of existing models was examined by comparing the tests data with the results predicted from existing failure pressure evaluation models for locally wall-thinned elbow.

• 대한기계학회논문집
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• 제19권6호
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• pp.1451-1459
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• 1995

The objective of this paper is to evaluate the material properties of SA312 TP316 and SA312 TP304 stainless steels and their associated welds manufactured for safety injection system of Yonggwang 3,4 nuclear generating stations. A total of 62 tensile tests and 46 fracture toughness tests were conducted and the effects of various parameters such as pipe size, crack plane orientation, tests were conducted and the effects of various parameters such as pipe size, crack plane orientation, test temperature, welding on material properties were discussed. Test results show that the effect of test temperature on fracture toughness was significant while the effects of pipe size and crack plane orientation on fracture toughness were negligible. Fracture toughness of the weld metal was in general higher than that of the base metal.

• 한국정밀공학회지
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• 제26권3호
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• pp.113-121
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• 2009

Behavior of a package of a microwave oven under the clamping condition is evaluated by tests and the finite element analyses. PAM-CRASH software is used for the finite element analyses. Results of the analyses are compared with those of the tests and accuracy is shown to be favorable. Under the clamping condition of the original design, severe deformation occurs and an improved design of the outer case and upper EPS(Expandable Poly Styrene) is proposed to reduce it. Face beads of the outer case are introduced and shape of the upper EPS is modified to reduce the deformation resulting from the clamping load. The improved design model is analyzed and its deformation is shown to be satisfactory. A prototype is produced according to the improved design and tests are performed. Results of the clamping test of the prototype show that the plastic deformation is removed totally.

• International Journal of Concrete Structures and Materials
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• 제3권2호
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• pp.91-95
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• 2009

Reclaimed asphalt pavement (RAP) is abundant substitute for natural aggregate in many areas. It is obtained by crushing of old road pavements in milling machine during rehabilitation and reconstruction process. In this study, reclaimed asphalt pavement mortars (RAPM) have been produced with different cement dosages and replacement ratios. The destructive and nondestructive tests have been conducted on specimens to determine physical and mechanical properties of RAPM. The free and restrained shrinkage tests on RAPM have been conducted to predict fractural behavior of mortars. The aim of the shrinkage tests was to delay crack formation and improve strain capacity of mortars before cracking. The results showed that RAPM exhibits lower elasticity modulus; however the tensile capacity was improved for deformation before cracking.

• 대한기계학회논문집A
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• 제23권7호
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• pp.1104-1111
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• 1999

A brake pedal for the flight control system of the Korean primary trainer is developed using composite material. The development includes the structural design, stress analysis, manufacturing and the qualification tests. A FEM analysis is used for the structural design and stress analysis. Autoclaving process is used to fabricate the composite brake pedal. For the qualification tests, modular fixtures are developed and applied. It is shown that the composite brake pedal developed meets all the structural integrity requirements specified in the military specification for aircraft parts.

• 대한기계학회논문집A
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• 제30권2호
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• pp.210-218
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• 2006

This paper has performed static, fatigue and nondestructive test of tilting' bolster frame for Korean tilting train. From the static test, the structural safety was investigated using Goodman diagram. After the static test, the fatigue test were conducted under tilting load conditions. The fatigue test was conducted for $10\times10^6$ cycles. During the fatigue test, the nondestructive tests using magnetic particle and liquid penetrant were performed at $6\times10^6$cycle and $10\times10^6$cycle. From the crack detection tests, it was known that there was no fatigue crack in the tilting bolster.