• Wind and Structures
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• 제19권4호
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• pp.421-441
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• 2014

With the assistance of typhoon field data at aerial elevation level observed by meteorological satellites and wind velocity and direction records nearby the ground gathered in Guangzhou Weather Station between 1985 and 2001, some key wind field parameters under typhoon climate in Guangzhou region were calibrated based on Monte-Carlo stochastic algorithm and Meng's typhoon numerical model. By using Peak Over Threshold method (POT) and Generalized Pareto Distribution (GPD), Wind field characteristics during typhoons for various return periods in several typical engineering fields were predicted, showing that some distribution rules in relation to gradient height of atmosphere boundary layer, power-law component of wind profile, gust factor and extreme wind velocity at 1-3s time interval are obviously different from corresponding items in Chinese wind load Codes. In order to evaluate the influence of typhoon field parameters on long-span flexible bridges, 1:100 reduced-scale wind field of type B terrain was reillustrated under typhoon and normal conditions utilizing passive turbulence generators in TJ-3 wind tunnel, and wind-induced performance tests of aero-elastic model of long-span Guangzhou Xinguang arch bridge were carried out as well. Furthermore, aerodynamic admittance function about lattice cross section in mid-span arch lib under the condition of higher turbulence intensity of typhoon field was identified via using high-frequency force-measured balance. Based on identified aerodynamic admittance expressions, Wind-induced stochastic vibration of Xinguang arch bridge under typhoon and normal climates was calculated and compared, considering structural geometrical non-linearity, stochastic wind attack angle effects, etc. Thus, the aerodynamic response characteristics under typhoon and normal conditions can be illustrated and checked, which are of satisfactory response results for different oncoming wind velocities with resemblance to those wind tunnel testing data under the two types of climate modes.

• 한국항공우주학회지
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• 제30권3호
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• pp.37-45
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• 2002

옆미끄럼이 있는 조건에서 LEX를 갖는 $65^{\circ}$ 후퇴각 삼각날개의 와류와 공력 특성을 실험적으로 연구하였다. 자유 유동속도는 40m/sec이고 이 속도와 날개뿌리 시위를 기준으로 한 단위길이당 레이놀즈 수는 $1.76{\times}10^6$이다. 받음각 범위는 $12^{\circ}$ 부터 $28^{\circ}$ 까지 이고, 시험된 옆미끄럼각은 $0^{\circ}$ , $-10^{\circ}$ , $-20^{\circ}$ 이다. 날개의 바람쪽에 있는 LEX 와류는 바람 반대쪽 LEX 와류보다 훨씬 더 강하고 날개면에 더 가깝게 날개 후류영역으로 진입한다. LEX 와류와 날개 와류는 서로 연동하여 집중되고 강한 와류를 형성하거나 날개 하류지역에서 붕괴된다. LEX 와류와 날개 와류의 상호작용으로 인하여 바람쪽 날개면에는 높은 흡입압력이 유지되고, 바람 반대쪽 날개면에는 낮은 흡입압력이 형성된다.

• 한국소음진동공학회논문집
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• 제15권12호
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• pp.1389-1397
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• 2005

Since blast-induced vibration may cause serious problem to the rock mass as well as the nearby structures, the prediction of blast-induced nitration and the stability evaluation must be performed before blasting activities. Dynamic analysis has been increased recently in order to analyze the effect of the blast-Induced vibration. Most of the previous studies, however, were based on the continuum analysis unable to consider rock joints which significantly affect the wave propagation and attenuation characteristics. They also adopted pressure corves estimated tv theoretical or empirical equations as input detonation load, thus there were very difficult to reflect the characteristics of propagating media. In this study, therefore, we suggested a dynamic distinct element analysis technique which uses velocity waveform obtained from a test blast as an input detonation load. A distinct element program, UDEC was used to consider the effect of rock joints. In order to verify the validity of proposed method, the test blast was simulated. The predicted results from the proposed method showed a good agreement with the measured vibration data from the test blast. Through the dynamic numerical modelling on the planned road tunnel and slope, we evaluated the effect of blast-induced nitration and the stability of rock slope.

• 설비공학논문집
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• 제21권9호
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• pp.519-526
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• 2009

Environmental control system is adopted to control the thermal load from the avionic equipment in the reconnaissance pod which is mounted under a fighter aircraft, undergoing large and rapid environmental changes with the variations of flight altitude and velocity. In this study, an environmental control system was designed and built by adopting vapor compression cycle using R-124. The cooling performance characteristics of the system were measured varying operating parameters: thermal load in the pod, air mass flow rate through evaporator, condenser inlet air temperature, and air mass flow rate through condenser. The effects of the experimental parameters on the system performance were analyzed based on the experimental results. The problems on the designed system were also analyzed and the solutions were suggested to improve system efficiency and to obtain stable operation.

• 대한조선학회논문집
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• 제31권4호
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• pp.66-72
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• 1994

선박의 조종성능을 정확히 평가하기 위해서 지난 약 10년간 각종모형시험이 수행되었다. 그러나 수학모델에 나타나는 변수들은 너무 다양하고, 복잡한 특성을 나타내기 때문에 아직까지 설계분야에 직접 사용할 수 있는 유용한 형태가 구축되지 않았다. 본 연구에서는, 이 수학모델에서 가장 중요한 변수인 프로펠러에서의 유효반류계수($1-{\omega}_P$)와, 유효타각 $\delta_R(\beta_R)$)을 회류수조에서 조사하였다. 모델은 설계속도와 저속에서 각각 실험이 이루어졌고, 흘수 또한 만재상태와 밸러스트상태에서 실시되었다. 프로펠러 추력과 타직압력은 주어진 사항각과 프로펠러 회전수에서 측정되었다. 이 추력은 유효유입속도나 유입방향의 해석에 사용된다.

• 한국항공우주학회지
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• 제43권12호
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• pp.1071-1078
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• 2015

외부형 핀틀추력기의 핀틀 행정거리, 고도, 보어유무가 핀틀추력기 성능에 미치는 영향에 대해서 전산수치해석을 수행하였다. 유동은 핀틀 행정거리에 관계없이 항상 과소팽창하는 결과를 보였다. 핀틀추력기의 주요 성능 지표 중 추력조절측면에서는 우수한 성능을 보였지만, 핀틀 지지대 윗면에서 발생한 충격파로 인해 공력하중이 증가하였다. 지상에서 고도 20 km로 상승하면 노즐 출구 속도, 마하수, 추력 등이 증가하였으며, 공력하중 또한 증가하였다. 보어의 존재는 공력하중을 5.9% 증가시켜 핀틀의 구동력을 위해서는 보어가 없는 형상이 유리하다고 판단된다.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2003년도 하계학술대회 논문집 Vol.4 No.2
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• pp.664-668
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• 2003

Transducer for ultrasonic linear motor with the symmetric and anti-symmetric modes was studied. The ultrasonic linear motor consists of two Langevin type piezoelectric vibrators that cross at right angles with each other in tip. In order to excite symmetric and anti-symmetric modes, the transducer must have a phase shift of 90 degree in space and time. Therefore, the tip of transducer moves on an elliptical motion. In this paper, the finite element analysis was used to optimize dimension and displacement of the transducer. The ultrasonic motor was fabricated using the simulated result and the driving characteristics were measured. No-load velocity was 0.28[m/s] and the maximum efficiency was 30[%] in resonance frequency.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2005년도 추계학술대회 논문집
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• pp.113-117
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• 2005

In the modern days, a galvannealed sheet steel (GA) instead of a cold rolled steel sheet has been widely used as an alternative to extend the life of automotive body. Accordingly, the mechanical properties of GA for automobiles were taken into account and studied by comparing with the temperature variation on annealing in this study. To clarify the effect of surface features in the mechanical and frictional properties of GA, the several tests such as nanoindentation, victors hardness and nano scratch test were executed. The developed neural networks apply also to obtain reliable mechanical properties of the thin films. Load-displacement curve was computed by the analysis procedure and compared with experimental results. The frictional characteristics of coating layers in GA were verified though nano scratch test in this study. The friction coefficient of coating layers on the surface was obtained from the nano scratch. The variation of friction coefficient versus velocity and pressure was taken into consideration in this paper.

• 한국주조공학회지
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• 제24권6호
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• pp.323-330
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• 2004

This study aims to investigate on the effects of the microstructures on the wear characteristics of the different grey cast iron(GC) and spheroidal ductile cast iron(DCI). Wear test using wear tester of pin-on-disc type was carried out under the conditions of load 47.2N , velocity 0.2m/s, distance 4000m. At the GC, Wear rates depend on graphite type and oxide layer formed at wear surface. Weak rosette graphites are easily broken and formed wear debris over 30 ${\mu}m$. This wear debris occurs scuffing at wear surface. As a result of surface deformation, Narrow regions of the matrix between the graphite flakes and the contact surface lead to the failure of the necks. Wear rate for the DCI depended on hardness of matrix more than size of graphite.

• Journal of Advanced Marine Engineering and Technology
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• 제28권1호
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• pp.152-161
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• 2004

The thermal load is a very important problem to be solved in many industrial systems including the electronic equipment. Impinging Jets have been known to provide a large heat transfer rates on surface for many years. The turbulence enhancement of fluid flow is requested for the efficiency elevation of heat transfer. A study on flow fields by rods attached to the wall surface as a promoter of turbulence enhancement has been carried out. The exact analysis on chracteristics of impinging jet field is requested to obtain the optimum design of the impinging jet system. By visualizing the flow field and processing the high digital image by computer PIV can afford exact data on the velocity vector kinetic energy and turbulence intensity in the complex turbulence field. In this study. three kinds of rod shape such as square. triangle. and semicircle are selected as the turbulence promoter. Nozzle diameters are 10mm. 17mm. and 23mm. And the analysis of the flow characteristics due to the above rods is carried out at Re No. 2.000, 3.000. and 4,000 by PIV measurement. It is clarified that the rod setup is very useful to obtain the turbulence enhancement and the turbulence intensity according to the shapes of rod appears large in order of the shapes of rod such as square 〉 triangle 〉semicircle.