• 대한물리의학회지
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• 제17권2호
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• pp.11-20
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• 2022

PURPOSE: This study investigated the immediate effects of gluteus medius strengthening training and relaxation therapy on the static balance, muscle strength asymmetry, and proprioception. METHODS: In this research, 38 healthy adults were assigned randomly to strengthening groups (SG) and relaxation groups (RG). The static balance, muscle strength asymmetry, and proprioception were measured as a pre-measurement. The same measurements were performed after the intervention and follow-up. An independent sample t-test was used to compare each group, and one-way repeated ANOVA was used to compare the changes within the group. RESULTS: In the static balance, the comparison between groups SG was more significant than RG, and only SG showed significant differences in the intra-group comparisons. There was no significant difference in muscle strength asymmetry between SG and RG. On the other hand, the comparison within the group revealed only SG to be significant. In proprioception, SG produced more significant results than RG, and only SG had significant values in the within-group comparison. CONCLUSION: Strengthening training affects the changes in static balance, muscle strength asymmetry, and proprioception.

• 한국지반공학회논문집
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• 제21권5호
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• pp.179-186
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• 2005

실내 모형실험으로 정,반복하중 재하 실험을 실시하여 하중과 침하, 지중 측방변위, 토목섬유 변위 등을 측정한 결과 지반과의 마찰과 토목섬유 인장력의 영향으로 전반적으로 지반의 변위가 줄고 지지력이 증가하였다. 또한 Mohr-coulomb 및 수정Mohr-Coulomb 모델들과 FLAC 4.0 2D을 사용하여 수치해석을 실시하였고 실내 모형 실험결과와 비교하였다. 기존식들은 토목섬유 모델링시 FLAC의 케이블 요소는 하중증가에 따른 전단강도를 증가되는 특성을 고려할수 없었기 때문에 실험 결과치와 상이하게 나타났다. 따라서 본 연구에서는 반복적인 학습으로 상재 하중의 영향을 고려한 케이블 구성요소의 적절한 식을 제시하였다.

• The Journal of Korean Physical Therapy
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• 제18권5호
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• pp.43-51
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• 2006

Purpose: The purpose of this study was to examine the effects of static stretching and Evjenth-Hamberg stretching on isokinetic muscle strength of knee flexors and extensors. Methods: The subjects were composed of eighty healthy males without weight-training experience. ROM of knee joint measured active maximal extension and isokinetic Peak Torque measured $60^{\circ}/sec,\;120^{\circ}/sec$ using an the En-Knee. Three tests(Baseline, 4 weeks, 8 weeks, respectively) was operated to examine change of each variable. Data were analyzed with a $2{\times}3$ analysis of variance ($group{\times}test$) for repeated measures on last factor by SPSS package 10.0. The data analysis revealed muscle strength were dependent on stretching method. Results: The results were as follows. First, Evjenth-Hamberg stretching(E-HS) was more effective than static stretching(SS) on ROM. Second, Peak Torque of knee flexors and extensors was improved in both methods by each time. but E-HS was more improved than SS. Conclusion: In conclusion, This study indicates that E-HS is more efficient than SS on muscle strength improvement.

• 한국정밀공학회지
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• 제18권6호
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• pp.59-66
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• 2001

Fatigue strength of the welding structure is governed by the residual stress at the weldment toe and static tensile overloads were known as relieving the residual stresses. In this study, static tensile overloads were applied to the welding structures which caused the relief of residual stresses. The amount of residual stress relief was found as proportional to the change of fatigue limit at the given conditions. Based on the fact of the proportionality between the change of fatigue limit and that of residual stress, simple measurement technique is proposed. Modified stress-life curves base on proposed technique gave good agreement with test results.

• 항공우주기술
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• 제3권1호
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• pp.27-34
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• 2004

50m 무인 비행선 비아50의 주 구조물인 꼬리날개, 곤돌라, 추력모터마운트(EMS) 등은 탄소 및 유리 섬유 복합재를 이용하여 설계/제작되었다. 사용된 재료 시편 강도 시험을 수행하여 설계 물성치를 확정하였다. 각각의 구조물들에 대하여 정하중 시험을 수행하여 구조 건전성을 입증하였다. 각 단품별로 정하중 시험을 수행하였으며, 보다 정확한 시험을 위하여 조립상태를 고려한 경계조건을 모사하였다. 100% DLL에서 영구변형이 발생하지 않음을 보였고, 150% DLL에서 파손이 발생하지 않음을 입증하였다.

• 한국항공운항학회지
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• 제20권1호
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• pp.103-111
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• 2012

This study reviews several fracture models for predicting the residual strength of notched composite laminates. Representative experimental results on the residual strength of composite laminates containing a notch subjected to static uniaxial tensile loading have been collected from open literature. And notched strength data for T300/5208 are analyzed. The various parameters associated with the fracture models have been determined for laminates. Notched strength data sets are compared with fracture models and the applicability of the different fracture models in predicting the notched strength of composite laminates is discussed. And static tests have been performed on 2.0mm depth notched specimen. And the test results are compared with analysis models.

• The Journal of Advanced Prosthodontics
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• 제8권5호
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• pp.388-395
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• 2016

PURPOSE. The purpose of this study was to evaluate the resistance to deformation under static overloading by measuring yield and fracture strength, and to analyze the failure characteristics of implant assemblies made of different titanium grades and connections. MATERIALS AND METHODS. Six groups of implant assemblies were fabricated according to ISO 14801 (n=10). These consisted of the combinations of 3 platform connections (external, internal, and morse tapered) and 2 materials (titanium grade 2 and titanium grade 4). Yield strength and fracture strength were evaluated with a computer-controlled Universal Testing Machine, and failed implant assemblies were classified and analyzed by optical microscopy. The data were analyzed using the One-way analysis of variance (ANOVA) and Student's t-test with the level of significance at P=.05. RESULTS. The group $IT4_S$ had the significantly highest values and group IT2 the lowest, for both yield strength and fracture strength. Groups $IT4_N$ and ET4 had similar yield and fracture strengths despite having different connection designs. Group MT2 and group IT2 had significant differences in yield and fracture strength although they were made by the same material as titanium grade 2. The implant system of the similar fixture-abutment interfaces and the same materials showed the similar characteristics of deformation. CONCLUSION. A longer internal connection and titanium grade 4 of the implant system is advantageous for static overloading condition. However, it is not only the connection design that affects the stability. The strength of the titanium grade as material is also important since it affects the implant stability. When using the implant system made of titanium grade 2, a larger diameter fixture should be selected in order to provide enough strength to withstand overloading.

• 한국구조물진단유지관리공학회 논문집
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• 제12권1호
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• pp.109-116
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• 2008

탄소섬유시트의 부착성능을 조사하는 방법으로써 중앙을 절단한 보 공시체를 이용한 휨 거동 형식의 시험기를 개발하여, 콘크리트의 압축강도를 변수로 정적 재하 실험을 실시하였다. 탄소섬유시트의 파단의 결과를 이용하여 이 시험기의 검증과 함께 전단부착강도의 산출식을 도출하려고 노력 하였다. 그 결과, 첫 번째로 새로운 형식의 시험기에 의한 부착강도시험의 타당성이 증명되었다. 두 번째는 CFS 표면 변형률의 결과로부터 구해진 전단부착강도는 2종류의 경향이 있음이 발견되었다. 그 데이터 중에서 비교적 안정성이 높은 전단부착강도의 평균치는 3.41MPa, 하한치는 2.11MPa이었다. 이번 실험에서는 콘크리트의 강도가 전단부착강도에 미치는 특별한 영향을 볼 수 없었다.

• 한국공작기계학회논문집
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• 제12권1호
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• pp.32-37
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• 2003

Evaluation of fatigue strength on the spot welded part is very important for strength design of spot welded steel structures. In this paper, we could get the life cycle of the spot welded part using the lethargy coefficient obtained through the quasi-static tensile shear test for the specimen welded by current 10kA. The reliability evaluation of the life cycle is completed by comparing the life cycle calculated under the constant loading rate with the life cycle obtained by dynamic fatigue test. And then the result calculated by the lethargy coefficient is verified through the lift cycle calculated using the dynamic final tensile stress formula under the increased loading speed. This way can make save the time and cost in processing of predicting the life cycle of a structure.

• 한국유체기계학회 논문집
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• 제17권4호
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• pp.11-18
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• 2014

The recent high speed propeller with blade sweep is required to have high strength to get the thrust to fly at high speed. The high stiffness and strength carbon/epoxy composite material is used for the major structure and skin-spar-foam sandwich structural type is adopted for advantage in terms of the blade weight. As a design procedure for the present study, the structural design load is estimated through investigation on aerodynamic load and then flanges of spars from major bending loads and the skin from shear loads are sized using the netting rule and Rule of Mixture. In order to investigate the structural safety and stability, stress analysis is performed by finite element analysis code MSC. NASTRAN. It is found that current methodology of composite structure design is a valid method through the static structural test of prototype blade.