• 터널과지하공간
• /
• 제19권6호
• /
• pp.567-582
• /
• 2009

일본의 기후현의 카미오카광산은 지하 약 1,000 m의 대심도에, 우주에서 도래하는 소립자의 관측과 양자의 붕괴현상 등을 연구하기 위한 실험시설 SUPER-KAMIOKANDE가 건설되었다. 이 시설 설계를 위한 기초 자료의 하나로, 초기지압 측정을 실시하여 건설 예정지의 암반 응력 상태를 파악했다. 측정 방법은, 일본 전력중앙연구소(Central Research Institute of the Electric Power Industry)에서 개발한 ８성분 변형률 게이지를 이용한 공경변화법, Sugahara와 Obara가 개발한 16성분 구면 게이지를 이용한 구면 공저변형법, 오스트레일리아의 CSIRO에 의해 개발된 Hollow Inclusion Cell을 이용한 공벽변형률법이다. ３종류의 방법에 의해 얻어진 결과가 일치하지는 않았지만, ６응력성분의 평균치를 이용하여 주응력 방향 및 크기를 결정하였다.

• Wind and Structures
• /
• 제6권6호
• /
• pp.485-498
• /
• 2003

This paper presents a mechanical model of Rain-Wind Induced Vibration (RWIV) of stay cables. It is based on the physical interpretation of the phenomenon as given in Cosentino, et al. (2003, referred as Part I). The model takes into account all the main forces acting on cable, on the upper water rivulet (responsible of the excitation) and the cable-rivulet interaction. It is a simplified (cable cross-sectional and deterministic) representation of the actual (stochastic and three-dimensional) phenomenon. The cable is represented by its cross section and it is subjected to mechanical and aerodynamic (considering the rivulet influence) forces. The rivulet is supposed to oscillate along the cable circumference and it is subjected to inertial and gravity forces, pressure gradients and air-water-cable frictions. The model parameters are calibrated by fitting with experimental results. In order to validate the proposed model and its physical basis, different conditions (wind speed and direction, cable frequency, etc.) have been numerically investigated. The results, which are in very good agreement with the RWIV field observations, confirm the validity of the method and its engineering applicability (to evaluate the RWIV sensitivity of new stays or to retrofit the existing ones). Nevertheless, the practical use of the model probably requires a more accurate calibration of some parameters through new and specifically oriented wind tunnel tests.

• 대한기계학회논문집B
• /
• 제30권2호
• /
• pp.136-143
• /
• 2006

A particle image velocimetry (PlV) technique has been applied to measure the quantitative flow field characteristics behind a road vehicle with/without an air spoiler attached on its trunk and to estimate its effect on the wake. A vehicle model scaled in the ratio of 1/43 is set up in the mid-section of a closed-loop water tunnel. The Reynolds number based on the vehicle length is $10^5$. To investigate the three-dimensional structure of the recirculation zone and vortices, measurements are carried out on the planes both parallel and perpendicular to the free stream, respectively. The results show significant differences in the recirculation region and the vorticity distributions according to the existence of the air spoiler. The focus and the saddle point, appearing just behind the air spoiler, are disposed differently along the spanwise direction. Regarding the streamwise vortices, the air spoiler produces large wing tip vortices. They have opposite rotational directions to C-pillar vortices which are commonly observed in case that the air spoiler is absent. The wing tip vortices generate the down-force and as a result, they can make the vehicle more stable in driving.

• 터널과지하공간
• /
• 제13권3호
• /
• pp.169-179
• /
• 2003

암석의 절리면 전단강도의 이방성을 연구하기 위하여 인공절리면을 형성한 시편에 대한 실험을 실시하고 그 결과를 분석하였다. 즉 낮은 수직응력 상태에서 전단 방향에 따른 전단강도, 전단강성 및 마찰각을 구하기 위한 실험을 실시하였다 그 결과 낮은 수직응력하에서 전단 강도 및 강성은 전단 방향에 따라 이방성을 보이며, 특히 수직응력 2.45 MPa미만에서 뚜렷하였다. 그리고 수직응력이 증가할수록 절리면의 이방성 효과는 감소하였다. 따라서 낮은 수직응력 하에서 전단강도 및 강성값을 보다 정확히 구하기 위해서 Barton의 식에 전단방향을 고려한 보정함수 F(a)를 반영하여 새로이 수정식을 제안한다.

• 항공우주기술
• /
• 제2권2호
• /
• pp.1-10
• /
• 2003

비행선은 주익이 없고 미익에 비해 동체 효과가 큰 형상 특성으로 인해 정적으로 불안정한 특성을 지닌다. 따라서 동안정 특성 예측이 매우 중요하다. 본 연구에서는 강제진동 풍동시험을 통한 비행선의 동안정 특성을 확보하였다. 풍동시험은 미국 BAR사의 독일소재 시설인 BAR LAMP 시설을 사용하였으며, 16회의 정적시험과 26회의 강제진동시험을 수행하였다. 시험결과, 비행선의 동안정 특성은 받음각 뿐만 아니라 옆미끄럼각, 각속도 크기와 방향에 비선형적으로 변한다. 전반적으로 세 방향의 모멘트는 댐핑이 있는 것으로 나타났으며, 수직력과 측력, 교차성분은 불안정하게 나타났다. 조종면의 영향은 작은 것으로 나타났으나 옆미끄럼각의 영향은 완전히 비선형적으로 나타났다.

• 한국유체기계학회 논문집
• /
• 제2권4호
• /
• pp.48-56
• /
• 1999

For the study on loss coefficients of turbine cascade with variation of incidence angle, the wind-tunnel tests were performed under the ranges in velocity of 10 m/s, 15 m/s, 20 m/s and incidence angles from $-20^{\circ}\;to\;20^{\circ}$ by intervals of $5^{\circ}$. Comparing our results with Soderberg's prediction, differences in loss coefficient were $2.5\%\;and\;2.8\%$ each for 10 m/s and 15 m/s. A large disagreement of $30.3\%$ was showed at 20 m/s freestream velocity. The comparisons of these test results with Ainley's prediction showed an $8\%$ difference in the case of 20 m/s freestream velocity. Test results were approximately comparable with Ainley's loss prediction's in incidence angles. Generally, averaged total pressure loss seemed to be decreased as Reynolds number increased. The total pressure loss coefficients were increased parabolically, as incidence angles were increased negatively and positively from $0^{\circ}$, in all speed ranges. At the far low freestream velocities, minimum loss accurred between $-5^{\circ}\;and\;+5^{\circ}$. But this minimum range narrowed the location of this range by shifting to the direction of the angle as freestream velocity was increased.

• 터널과지하공간
• /
• 제20권3호
• /
• pp.217-224
• /
• 2010

비교적 균질한 3가지 화강암이 암석의 미세구조적 특성과 파괴인성 사이의 관계를 조사하기 위하여 연구되었다. 광학 현미경 관찰로 분석된 광물입자의 장축과 미세균열의 방위에 의하여 파괴인성 및 초음파 속도의 변화를 보였다. 가장 작은 값을 나타내는 파괴인성은 인장응력 방향과 수직하게 발달된 광물입자의 장축 및 미세균열의 방향이 주결에 일치할 때로서 파괴가 연약면인 광물입자의 장축이나 미세균열의 우세방향에 평행하게 전달될 때이다. SR 시편으로 측정된 파괴인성값은 1.63~2.62 MPa $m^{0.5}$의 변화를 보이며, 그 값들은 광물입자의 평균크기 및 미세균열의 평균길이와 관련된다.

• 한국신재생에너지학회:학술대회논문집
• /
• 한국신재생에너지학회 2009년도 춘계학술대회 논문집
• /
• pp.516-520
• /
• 2009

This study describes aerodynamic characteristics for the HAWT (Horizontal Axis Wind Turbine) rotor blade using general CFD(Computational Fluid Dynamics) code. The boundary conditions for analysis are validated with the experimental result by the NREL (National Renewable Energy Laboratory)/NASA Ames wind tunnel test for S809 airfoil. In the case of wind turbine rotor blade, complex phenomena are appeared such as flow separation and re-attachment. Those are handled by using a commercial flow analysis tool. The 2-equation k-$\omega$ SST turbulence model and transition model appear to be well suited for the prediction. The 3-dimensional phenomena in the HAWT rotor blade is simulated by a commercial 3-D aerodynamic analysis tool. Tip vortex geometry and Radial direction flows along the blade are checked by the analysis.

• 한국연소학회지
• /
• 제4권2호
• /
• pp.23-33
• /
• 1999

A turbulent non-premixed ethylene flame, which was set up in a vertical wind tunnel, was examined to understand the effect of turbulent mixing on formations of soot and gaseous species in the flames. Temperature and velocity profiles were measured using uncoated thermocouples and LDV system. Gaseous samples were withdrawn by using a water cooled stainless iso-kinetic gas sampling probe. The samples for inorganic compounds and light hydrocarbons were collected with sampling bottles and were analyzed by a gas chromatography. The samples for aromatic hydrocarbons were collected on a sorbent tube and were analyzed on a GC/MS system. Some of main results were followed. CO and $CO_2$ were measured relatively in early part of flame and the concentration of CO was greater than that of $CO_2$ all over the early flame region due to the scavenging of the oxidizing species OH by soot particles. Aromatic hydrocarbons were measured at x/D=122 along the radial direction and main important species were benzene, xylene, toluene, styrene, indene, naphthalene. The peak points of these compounds occurred at r/D=0.8 apart from the center of flame, around in which the concentration of $C_2H_2$ decayed relatively rapidly from the maximum value.

• 기술사
• /
• 제18권3호
• /
• pp.1-20
• /
• 1985

The traffic congestion of Seoul city has been one of the most serious problems to be settled since the advent of 1970s. As a means to mitigate traffic mess, the authority concerned launched the construction of subway line 3 and 4 in 1980. The two Subway lines slated for completion by 1985 cross each other and run north-south direction, passing through the metropolitan area of Seoul city fraught with high-rise edifices and large-scale shopping centers, and, in order to reduce blasting vibration, NATM was executed for a distance of 10 Km, instead of ASSM previously employed when subway line 1 and 2 were constructed. Tunnel blastings were implemented, preceded by classifying the rocks at construction area into five categories, namely, hard rock, semi-hard rock, weak rock weathered rock and silt and by calculating their respective specific charges through standard test blastings, by employing the pre-splitting and smooth blasting with drilling patterns of burn cut type, so as not to cause damages to surface structures. Most of explosives used were the slurry of low specific gravity and low velocity, and the firings executed by the use of milli-second detonators. Empiric formula were also formulated to check blasting vibrations, based on the vibration allowable values of West Germany standard, for the application to vulnerable construction zones. Should the two lines be placed for public service in 1985, about 40% of the total traffic population of Seoul city amounting to 15 million as of 1984 is estimated to be carried by subway with no difficulties.