• 한국유체기계학회 논문집
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• 제19권1호
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• pp.11-17
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• 2016

In this paper, a numerical analysis was performed to investigate the effect of the pitch angle of a helical nozzle on the performance characteristics of a vortex tube. Three-dimensional numerical simulation has been performed with standard $k-{\varepsilon}$ turbulence model by using FLUENT 13.0. The effect of the pitch angle of helical nozzle was described in term of ${\beta}$. A CFD analysis was performed on ${\beta}=0^{\circ}$, $5^{\circ}$, $10^{\circ}$, $15^{\circ}$. In order to realize the influence of ${\beta}$ on performances of the vortex tube. Computation results were expressed by the ${\beta}-{\Delta}T_{h,c}$ graph and radial profiles of axial velocity and swirl velocity. The results showed that ${\beta}$ which improves energy separation capacity of vortex tube was $5^{\circ}$ at ${\alpha}=0.33$, 0.5 and $10^{\circ}$ at ${\alpha}=0.33$. Besides, It was confirmed that the results were closely related to axial velocity and swirl velocity.

• 대한기계학회논문집
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• 제15권1호
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• pp.28-40
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• 1991

본 연구에서는 4변이 단순 지지된 두꺼운 역대칭 앵글 플라이 적층판의 굽힘, 좌굴 및 진동 거동을 규명하였으며, 인장과 굽힘, 비틀림 사이의 결합 특성을 고려하 였고, 전단 변형을 고려하였다.또 유사 변환 개념을 도입하여 복합 재료 적층판의 거동을 일반화 하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제34권1호
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• pp.69-75
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• 2010

본 연구는 Weis-Fogh형 추진기구를 장착한 모형선을 제작하여, 정지 및 주행하는 모형선에 대해 열림각 변화에 따른 주행특성과 진동특성을 조사한 것이다. 그 결과를 요약하면 다음과 같다. 추력 및 선속은 열림각이 자동 조절되는 스프링형이 가장 컸으며, 열림각 ${\alpha}=30^{\circ}$, ${\alpha}=15^{\circ}$순으로, 약 4%정도씩 작게 나타났다. 또한 모형선의 최대 진동진폭 및 RMS 값은 열림각 ${\alpha}=30^{\circ}$일 때가 가장 작게, 스프링형이 가장 크게 나타났고, 열림각이 같은 경우 정지 때보다 주행 시가 작게 나타났다.

• Geomechanics and Engineering
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• 제15권5호
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• pp.1113-1124
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• 2018

Geological dynamic hazards during deep coal mining are caused by the failure of a composite system consisting of the rock and coal layers, whereas the joint in coal affects the stability of the composite system. In this paper, the compression test simulations for the rock-coal combined body with single joint in coal were conducted using $PFC^{2D}$ software and especially the effects of joint length and joint angle on strength and failure characteristics in a rock-coal combined body were analyzed. The joint length and joint angle exhibit a deterioration effect on the strength and affect the failure modes. The deterioration effect of joint length of L on the strength can be neglected with a tiny variation at ${\alpha}$ of $0^{\circ}$ or $90^{\circ}$ between the loading direction and joint direction. While, the deterioration effect of L on strength are relatively large at ${\alpha}$ between $30^{\circ}$ and $60^{\circ}$. And the peak stress and peak strain decrease with the increase of L. Additionally, the deterioration effect of ${\alpha}$ on the strength becomes larger with the increase of L. With the increase of ${\alpha}$, the peak stress and peak strain first decrease and then increase, presenting "V-shaped" curves. And the peak stress and peak strain at ${\alpha}$ of $45^{\circ}$ are the smallest. Moreover, the failure mainly occurs within the coal and no apparent failure is observed for rock. At ${\alpha}$ between $30^{\circ}$ and $60^{\circ}$, the secondary shear cracks generated in or close to the joint tips, cause the structural instability failure of the combined body. Therefore, their failure models present as a shear failure along partial joint plane direction and partially cutting across the coal body or a shear failure along the joint plane direction. However, at ${\alpha}$ of $60^{\circ}$ and L of 10 mm, the "V-shaped" shear cracks cutting across the coal body cause its final failure. While crack nucleations at ${\alpha}$ of $0^{\circ}$ or $90^{\circ}$ are randomly distributed in the coal, the failure mode shows a V-shaped shear failure cutting across the coal body.

• 한국안광학회지
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• 제6권2호
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• pp.65-70
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• 2001

두 개의 토로이드 면이 서로 직각인 토릭렌즈의 두 곡률의 합($C_x+C_y$)는 $$C_x+C_y=\frac{x^2+y^2}{2r_1}+\frac{x^2}{2}(\frac{1}{r_2}-\frac{1}{r_1})$$이며, 사축인 토릭렌즈의 두 곡률의 합 ($C_a+C_b$)은 $$(C_a+C_b)=\frac{x^2cos^2{\alpha}_1}{2r_1}+\frac{x^2cos^2{\alpha}_2}{2r_2}+\frac{y^2sin^2{\alpha}_1}{2r_1}+\frac{y^2sin^2{\alpha}_2}{2r_2}$$이다. $(C_1+C_2)+(C_1+C_2)_{90^{\circ}}$는 구면의 곡률 합$S_{S_1}+S_{S_2}$과 같은 값을 얻었다. 표면 곡률(Cx, Cy) 값을 포함한 사축 토릭렌즈의 합성 굴절력의 parameter S, C, ${\theta}$ 값을 다음과 같다. $$S=(n-1)\[\frac{C_x}{x^2}+\frac{C_y}{y^2}\]-\frac{C}{2},\;C=-\frac{2(n-1)}{sin2{\theta}}\[\frac{C_x}{x^2}+\frac{C_y}{y^2}\]$$ $${\theta}=\frac{1}{2}tan^{-1}\[-\frac{{C_xy^2sin2{\theta}_1}+{C_yx^2sin2{\theta}_2}}{{C_xy^2cos2{\theta}_1}+{C_yx^2cos2{\theta}_2}}\]$$.

• Wind and Structures
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• 제7권1호
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• pp.41-54
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• 2004

An analysis refinement of the Messina Strait suspension bridge project has been recently required, concerning mainly the yaw angle effects on the multi-box deck section aerodynamics and the vortex shedding at low reduced velocities $V^*$. In particular the possible interaction of the axial flow with the large cross beams has been investigated. An original test rig has been designed at this purpose allowing for both forced motion and free motion aero elastic tests, varying the average angle of attack ${\alpha}$ and the deck yaw angle ${\beta}$. The hydraulic driven test rig allowed for both dynamic and stationary tests so that both the stationary coefficients and the flutter derivatives have been evaluated for each yaw angle. Specific free motion tests, taking advantage from the aeroelastic features of the section model, allowed also the study of the vortex shedding induced phenomena.

• 한국운동역학회지
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• 제31권1호
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• pp.44-49
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• 2021

Objective: The purpose of this study was to analyze kinematic variables according to ground slope angle during golf putting. Method: 26 collegiate golfers (age: 22.54±2.15 kg, height: 174.64±6.07 cm, weight: 71.35±9.27 kg, handicap: 5.11±4.50) were participated, and 8 motion capture cameras (250 Hz), Nexus, and Kwon3DXP software were used to collect data. It was performed repeated measures ANOVA and Bonferroni adjustment. Alpha set at .05. Results: Body alignments were not significantly different at address. Putter head trajectory and loft angle were significantly different, and AP direction of acceleration of putter head was significantly different. However, ML and SI direction of acceleration of putter head were not significantly different. Conclusion: Therefore, it was identified that ground slope angle was affected the kinematic variables during putting, and it will be performed that correlation analysis between putting success rate and kinematic variables according to ground slope angle during golf putting.

• 대한기계학회논문집B
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• 제34권1호
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• pp.45-52
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• 2010

본 연구에서는 Weis-Fogh 메카니즘의 원리를 응용한 수 종류의 추진모델을 간략하고, 이 추진모델을 기계화한 소위 Weis-Fogh 형 모형선을 제작하여, 추진모델 I, II, III의 주행특성과 진동특성을 비교, 검토함과 동시에, 탄성날개가 실선에서도 유효한지 주행실험을 통하여 파악한 것이다. 그 결과를 요약하면 다음과 같다. 추진모델 II에 대하여 추진모델 I 및 III의 추력은 각각 1.31배 및 1.43배의 크기로 발생했고, 선속은 각각 1.20배 및 1.23배 증가했다. 탄성날개를 이용한 추진력 개선은 실선에서도, 모든 추진모델에 대해서도 유효했다. 최대진폭 및 RMS값은 열림각 ${\alpha}=15^{\circ}$에서 가장 큰 값을 나타내며, 열림각 ${\alpha}=30^{\circ}$에서 가장 작게 나타났다. 출력성능 면에서 열림각 ${\alpha}=30^{\circ}$, 추진모델 III의 ${\Delta}T=0^{\circ}$의 경우가 비교적 추력이 크고, 진동특성도 우수했다.

• 한국지반공학회지:지반
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• 제10권1호
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• pp.63-70
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• 1994

수평지반내의 한 지점에 대한 원위치의 압밀상태는 $K_0$-이방압밀 되어있으며 토압계수 $K_0$값은 흙의 성질과 옹력이력에 따라 다르다. $K_0$-이방정규압밀점토지반의 원위치 비배수전단강도를 등방압밀시헙에 의해서 추정하기 위하여 4가지의 압밀응력비($K={\sigma}'_{3c}/{\sigma}'_{1c}$)로서 이방압밀시킨 비배수전단시험을 시행하여 ($S_u/{\sigma}'_{1c})_{CKU}=\alpha(S_u/{\sigma}'_{1c})_{CIU}$로 나타내는 강도비 $\alpha$와 압밀응력비 K의 관계를 나타내었다. 시험결과 강도비 $\alpha$는 압밀웅력비가 클수록 증가하고 내부마찰각$\Phi'$와 $\Phi'_{CKU}/\Phi'_{CIU}/$비도 압밀 응력비가 클수록 동시에 증가한다.

• 대한기계학회논문집B
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• 제28권7호
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• pp.789-799
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• 2004

An experimental study is conducted to investigate the effects of duct corrugation angle on heat/mass transfer characteristics in wavy ducts of a primary surface heat exchanger application. Local heat/mass transfer coefficients on the wavy duct sidewalls are determined by using a naphthalene sublimation technique. The corrugation angles(${\alpha}$) of the wavy ducts are 145$^{\circ}$, 130$^{\circ}$, 115$^{\circ}$ and 100$^{\circ}$. And the Reynolds numbers based on the duct hydraulic diameter vary from 300 to 3,000. The results show that at the low Re(Re $\leq$1000), the secondary vortices called Taylor-Gortler vortices perpendicular to the main flow direction are generated due to effect of duct curvature. By these secondary vortices, high heat/mass transfer regions are formed on both pressure-side and suction-side walls. At the high Re(Re $\geq$ 1000), these secondary flows are vanished with helping flow transition to turbulent flow and the regions which show high heat/mass coefficients by flow reattachment are formed on suction side. As corrugation angle decreases, the local peak Sh induced by Taylor-Gortler vortices increase at Re $\leq$1000. At high Re(Re $\geq$ 1000), by the existence of different kind of secondary flows called Dean vortices, non-uniform Sh distribution appears along spanwise direction at the narrow corrugation angle (${\alpha}$=100$^{\circ}$). Average Sh also increase by the enhanced effect of secondary vortices and flow reattachment. More pumping power (pressure loss) is required with the smaller corrugation angle due to the enhancement of flow instability.