• 제목/요약/키워드: longitudinal tunnel

검색결과 212건 처리시간 0.025초

스마트 무인기 TR-S2 형상의 정적 풍동시험 (Static Wind Tunnel Test of Smart Un-manned Aerial Vehicle(SUAV) for TR-S2 Configuration)

  • 최성욱;조태환;정진덕
    • 대한기계학회논문집B
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    • 제29권6호
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    • pp.755-762
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    • 2005
  • To evaluate the aerodynamic efficiency of TR-S2 configuration designed by SUDC, wind tunnel tests of $40\%$ scaled model were done in KARI LSWT. The aerodynamic characteristics of plain and Semi-Slotted Flaperon were compared, and vortex generators were installed to improve flow pattern along the wing surface. Effects of the control surface such as elevator, rudder, aileron, and incidence angle of horizontal tail are measured for various testing conditions. Test results showed that Semi-Slotted Flaperon produced more favorable lift, lift/drag, and stall margins and application of vortex generator would be best choice to enhance wing performance. Longitudinal, lateral and directional characteristics of TR-S2 were found to be stable for the pitch and yaw motions.

스마트 무인기 TR-S4 형상의 정적 풍동시험 (Static Wind Tunnel Test of Smart Un-manned Aerial Vehicle(SUAV) for TR-S4 Configuration)

  • 최성욱;김철완;이장연;정진덕
    • 대한기계학회논문집B
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    • 제30권10호
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    • pp.1012-1018
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    • 2006
  • To evaluate the aerodynamic efficiency of TR-S4 configuration, wind tunnel tests of 40% scaled model were done in KARI LSWT. TR-S4 configuration has different nacelle shape, larger EO/IR camera and aftward wing location compared with TR-S2. Component build-up test after adding each element of model is performed. Also effects of horizontal tail incidences, Flaperon and Aileron deflection. on aerodynamic characteristics are measured. Test results showed that TR-S4 configuration has favorable stability characteristics in longitudinal, lateral and directional for the pitch and yaw motions.

스마트 무인기 TR-E2S1 형상 풍동시험 결과 (Wind Tunnel Test of Smart Un-manned Aerial Vehicle(SUAV) for TR-E2S1 Configuration)

  • 윤성준;조태환;정진덕
    • 대한기계학회논문집B
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    • 제29권3호
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    • pp.295-305
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    • 2005
  • To improve the aerodynamic effciency of TR-E2, a new configuration so called TR-E2Sl was introduced. TR-2251 is composed of different wing airfoil section and T-tail shape compared with TR-E2. Wind tunnel test for TR-EBS1 had been performed by changing the incidence angles of wing and deflection angles of control surfaces such as elevator and rudder. Also the on/off effect of ventral fin attached underneath of AFT fuselage was tested. Test result showed that variations of wing incidence angle did not cause any severe differences in aerodynamic characteristics. Longitudinal and directional characteristics of TR-E2S1 show stable for the pitch and yaw motions. However, the lateral stability of TR-E2S1 is not stable for a certain control surface deflection.

도로터널내 화재 발생시 매연 제거를 위한 모델 해석 (A Model-Analysis for Removal of Fire Fumes in a Road Tunnel during a Fire Disaster)

  • 윤성욱;이희근
    • 터널과지하공간
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    • 제7권2호
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    • pp.100-107
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    • 1997
  • In case of a fire outbreak in a uni-directional road tunnel, the flow of traffic immediately behind the fire disaster will be stalled all the way back to the entrance of the tunnel. Furthermore, when the vehicle passengers try to flee away from the fire toward the entrance of the tunnel, the extremely hot fume that propagates in the same direction will be fatal to the multitudes evacuating, but may also cause damage to the ventilation equipments and the vehicles, compounding the evacuation process. This paper will present the 3-dimensional modelling analysis of the preventive measures of such a fume propagation in the same direction as the evacuating passengers. For the analysis, the fire hazard was assumed to be a perfect combustion of methane gas injected through the 1 m X 2 m nozzle in the middle of the tunnel, and the product of $CO_2$ as the indicator of the fume propagation. From the research results, when the fire hazard occurred in middle of the 400 m road tunnel, the air density decreased around the fire point, and the maximum temperatures were 996 K and 499 K at 210 m and 350 m locations, respectively, 60 seconds after fire disaster occurred, when the fumes were driven out only towards the exit-direction of the tunnel. By tracing the increase of $CO_2$ level over 1% mole fraction, the minimum longitudinal ventilation velocity was found to be 2.40 m/sec. Furthermore, through Analysis of the temperature distribution graphs, and observation of the cross-sectional distribution of $CO_2$ over 1% mole fraction, it was found that the fume did not mix with the air, but rather moved far in a laminar flow towards exit of the tunnel.

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터널 3차원 절대변위 해석기법을 이용한 막장전방지반 예측 (Prediction of Ground Condition Changes Ahead of Tunnel Face Using Three-Dimensional Absolute Displacement Analysis)

  • 방준호;한일영
    • 한국터널지하공간학회 논문집
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    • 제8권2호
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    • pp.101-113
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    • 2006
  • 안정된 암반에 터널을 굴착하는 경우 아칭효과에 의해 막장주변에 응력재배치가 발생하고 터널 막장 전방에 연약대가 존재하는 경우 응력재배치가 충분히 이루어지지 않아 막장과 연약대 사이의 응력집중으로 인해 변위가 발생하게 된다. 만일 막장에 근접하여 측점에서 종방향, 횡방향, 연직방향의 3차원 절대좌표가 측정되는 경우 막장전방의 지반거동이 반영된 3차원 절대변위가 산정되고, 이러한 3차원 절대변위의 분석을 통해 막장전방의 지반조건을 예측할 수 있게 된다. 본 연구에서는 4개 현장에서 측정된 3차원 변위비의 경향선과 천단침하의 영향선/경향선 분석을 실시하여 연약대 위치를 추정하였고, 3차원 절대변위의 분석에 의해 추정된 연약대 위치를 동일한 구간에서의 TSP탐사로 추정된 연약대 위치와 비교함으로써 3차원 절대변위 해석기법의 현장 적용성을 검증하였다.

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Probabilistic analysis of tunnel collapse: Bayesian method for detecting change points

  • Zhou, Binghua;Xue, Yiguo;Li, Shucai;Qiu, Daohong;Tao, Yufan;Zhang, Kai;Zhang, Xueliang;Xia, Teng
    • Geomechanics and Engineering
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    • 제22권4호
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    • pp.291-303
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    • 2020
  • The deformation of the rock surrounding a tunnel manifests due to the stress redistribution within the surrounding rock. By observing the deformation of the surrounding rock, we can not only determine the stability of the surrounding rock and supporting structure but also predict the future state of the surrounding rock. In this paper, we used grey system theory to analyse the factors that affect the deformation of the rock surrounding a tunnel. The results show that the 5 main influencing factors are longitudinal wave velocity, tunnel burial depth, groundwater development, surrounding rock support type and construction management level. Furthermore, we used seismic prospecting data, preliminary survey data and excavated section monitoring data to establish a neural network learning model to predict the total amount of deformation of the surrounding rock during tunnel collapse. Subsequently, the probability of a change in deformation in each predicted section was obtained by using a Bayesian method for detecting change points. Finally, through an analysis of the distribution of the change probability and a comparison with the actual situation, we deduced the survey mark at which collapse would most likely occur. Surface collapse suddenly occurred when the tunnel was excavated to this predicted distance. This work further proved that the Bayesian method can accurately detect change points for risk evaluation, enhancing the accuracy of tunnel collapse forecasting. This research provides a reference and a guide for future research on the probability analysis of tunnel collapse.

조개 표면의 종방향 그루브가 공력성능에 미치는 영향 (Effect of longitudinal grooves of the scallop surface on aerodynamic performance)

  • 김태훈;최해천
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회B
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    • pp.2419-2421
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    • 2008
  • Some of the scallops like Amesium balloti have an excellent level-swimming ability, i.e. they can swim about 20m by single level swimming with a maximum swimming velocity of about 1.6m/s in the sea. On the other hand, some species like Patinopecten yessoensis have longitudinal grooves on the upper and lower surfaces and others do not. Therefore, in the present study, we measure the lift and drag forces on a real scallop model (Patinopecten yessoensis) in a wind tunnel. Experiments are performed at the Reynolds number of 75,000 based on the maximum chord length, which is within the swimming condition of real scallop (Re = $30,000{\sim}300,000$). To see the effect of longitudinal grooves, we measure the aerodynamic forces on a scallop model by removing the grooves. With the grooves, the lift force increases at low angles of attack (${\alpha}<10^{\circ}$). The drag force increases slightly at all the attack angles considered. The lift-to-drag ratio is increased by about 10% at ${\alpha}<10^{\circ}$.

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전방십자인대 재건술시 대퇴골 터널에 있어 전내측 삽입구의 유용성 (Usefulness of Anteromedial Portal for Femoral Tunneling in Anterior Cruciate Ligament Reconstruction)

  • 강민수;김인보;김경택
    • 대한관절경학회지
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    • 제12권2호
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    • pp.118-124
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    • 2008
  • Purpose: Recent development and advances in the arthroscopic surgical techniques for anterior cruciate ligament(ACL) reconstruction have led to the ideal location for more oblique anatomic point of the femur from 10 to 10:30 o'clock(in the right knee) and from 2 to 1:30 o'clock(in the left knee) in the frontal plane. This study was performed to compare the operative methods and the radiologic results of the femoral tunnels made through the tibial tunnel(trans-tibial approach) and the anteromedial portal. Materials and Methods: From January 2003 to May 2004, on hundred reconstructions of ACL were performed. Group I(the femoral tunnel made through the tibial tunnel) consisted of 50 cases and group I(the femoral tunnel made through the anteromedial portal) consisted of 50 cases. The operative methods and the radiographic results of the femoral tunnels were compared. Results: Femoral tunnel was made more easily at more oblique anatomic point in group II than in group I. In group II, better visual field was achieved at the angle of 100? flexion of the knee joint, the risks of the posterior cortical breakage and the tunnel-graft mismatching were reduced more, and the divergence of femoral interference screw from the radiograph decreased more than in group I(p<0.05). The angle between the femoral tunnel and the longitudinal axis of ACL increased in group II. Conclusion: Anteromedial portal technique was useful for femoral tunneling toward 10 to 10:30 o'clock(in the right knee) and 2 to 1:30 o'clock(in the left knee) in ACL reconstruction. Level of Evidence:Level III, case-control study.

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파쇄대의 공간적 분포가 터널 거동에 미치는 영향 - 수치해석 연구 (Effect of orientation of fracture zone on tunnel behavior - Numerical Investigation)

  • 유충식;조윤규;박정규
    • 한국터널지하공간학회 논문집
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    • 제15권3호
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    • pp.253-270
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    • 2013
  • 본 연구에서는 파쇄대의 공간적 분포 특성이 터널의 거동에 미치는 영향에 대한 내용을 다루었다. 이를 위해 발파굴착 공법이 적용되는 터널을 대상으로 다양한 파쇄대 조건을 도출하고 이에 대한 2차원 및 3차원 해석을 수행하여 파쇄대의 주향 및 경사, 터널과의 이격거리, 토피고, 측압계수 등에 대한 매개변수 연구를 실시하였다. 해석결과를 토대로 매개변수 조건에 대한 터널 변위 및 지보재 부재력의 변화경향을 고찰하였으며 그 결과 파쇄대의 경사각 및 주향에 따라 터널의 변위 및 지보재 부재력에서 큰 차이를 보였으며 전반적으로 터널의 심도가 깊어질수록 그리고 초기측압계수가 클수록 파쇄대의 공간적 분포 특성에 따른 터널 거동의 차이가 더 심화되는 것으로 나타나 대심도 터널의 경우가 저심도 터널에 비해 파쇄대의 영향이 가중될 수 있는 것으로 검토되었다.

과도 액정 기법을 이용한 와동발생기 하류의 유동장 및 열전달 측정 (Detailed Measurement of Flow and Heat Transfer Downstream of Rectanglar Vortex Generators Using a Transient Liquid Crystal Technique)

  • 홍철현;양장식;이기백
    • 대한기계학회논문집B
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    • 제27권11호
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    • pp.1618-1629
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    • 2003
  • The effects of the interaction between flow field and heat transfer caused by the longitudinal vortices are experimentally investigated using a five hole probe and a transient liquid crystal technique. The test facility consists of a wind tunnel with vortex generators protruding from a bottom surface and a mesh heater. In order to control the strength of the longitudinal vortices, the angle of attack of vortex generators used in the present experiment is 20$^{\circ}$, and the spacing between the vortex generators is 25mm. The height and cord length of the vortex generator is 20mm and 50mm, respectively. Three-component mean velocity measurements are made using a f-hole probe system, and the surface temperature distribution is measured by the hue capturing method using a transient liquid crystal technique. The transient liquid crystal technique in measuring heat transfer has become one of the most effective ways in determining the full surface distributions of heat transfer coefficients. The key point of this technique is to convert the inlet flow temperature into an exponential temperature profile using the mesh heater set up in the wind tunnel. The conclusions obtained in the present experiment are as follows: The two maximum heat transfer values exist over the whole domain, and as the longitudinal vortices move to the farther downstream region, these peak values show the decreasing trends. These trends are also observed in the experimental results of other researchers to have used the uniform heat flux method.