• 한국통신학회논문지
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• 제36권3A호
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• pp.205-214
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• 2011

3GPP LTE (3rd Generation Project Partnership Long Tenn Evolution)에서는 SFN (Single Frequency Network) 환경에서 동일 데이터를 복수의 단말에 동시에 전송하는 무선 멀티캐스트 기술에 대한 연구가 활발하게 진행 중이다. 이러한 환경에서 효율적인 데이터 전송을 위해서는 멀티캐스트 커버리지 요구사항을 만족하는 최적의 전송 기법을 선택해야 하며 이를 위해 단말들의 수신 성능에 대한 정보가 반드시 필요하다. 하지만 실제 시스템에서 매 순간마다 모든 단말의 수신 성능을 피드백 받는 것은 상당한 역방향 링크의 채널자원을 필요로 한다. 이러한 문제를 해결하기 위해 본 논문에서는 단말의 수신 성능에 대한 예측을 바탕으로 멀티캐스트 커버리지를 예측하는 알고리즘을 제안하고 성능을 비교분석 하였다. 제안한 알고리즘은 각각의 단말이 자신의 수선 성공 여부 패턴에 따라 자신의 상태를 결정하고, 상태 천이 확률을 계산한다. 이를 일정한 주기 마다 기지국에 피드백하고, 기지국은 이러한 정보를 바탕으로 멀티캐스트 커버리지를 예측한다. 시뮬레이션을 통해 제안된 방법을 통한 커버리지 예측이 가능함을 확인하였다.

• Geomechanics and Engineering
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• 제28권3호
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• pp.265-281
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• 2022

A set of slurry shield test system capable of cutter cutting and slurry automatic circulation is used to investigate the deformation characteristics, the evolution characteristics of support resistance and the distribution and evolution process of earth pressure during excavating and collapsing of slurry shield tunneling in circular-gravel layer. The influence of cover-span ratio on surface subsidence, support resistance and failure mode of excavation face is also discussed. Three-dimensional numerical calculations are performed to verify the reliability of the test results. The results show that, with the decrease of the supporting force of the excavation face, the surface subsidence goes through four stages: insensitivity, slow growth, rapid growth and stability. The influence of shield excavation on the axial earth pressure of the front soil is greater than that of the vertical earth pressure. When the support resistance of the excavation face decreases to the critical value, the soil in front of the excavation face collapses. The shape of the collapse is similar to that of a bucket. The ultimate support resistance increase with the increase of the cover-span ratio, however, the angle between the bottom of the collapsed body and the direction of the tunnel excavation axis when the excavation face is damaged increase first and then becomes stable. The surface settlement value and the range of settlement trough decrease with the increase of cover-span ratio. The numerical results are basically consistent with the model test results.

• 천문학회보
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• 제45권1호
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• pp.38.2-38.2
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• 2020

Horizon Run 5 (HR5) is a cosmological hydrodynamical simulation which captures the properties of the Universe on a Gpc scale while achieving a resolution of 1 kpc. This enormous dynamic range allows us to simultaneously capture the physics of the cosmic web on very large scales and account for the formation and evolution of dwarf galaxies on much smaller scales. Inside the simulation box. we zoom-in on a high-resolution cuboid region with a volume of 1049 × 114 × 114 Mpc3. The subgrid physics chosen to model galaxy formation includes radiative heating/cooling, reionization, star formation, supernova feedback, chemical evolution tracking the enrichment of oxygen and iron, the growth of supermassive black holes and feedback from active galactic nuclei (AGN) in the form of a dual jet-heating mode. For this simulation we implemented a hybrid MPI-OpenMP version of the RAMSES code, specifically targeted for modern many-core many thread parallel architectures. For the post-processing, we extended the Friends-of-Friend (FoF) algorithm and developed a new galaxy finder to analyse the large outputs of HR5. The simulation successfully reproduces many observations, such as the cosmic star formation history, connectivity of galaxy distribution and stellar mass functions. The simulation also indicates that hydrodynamical effects on small scales impact galaxy clustering up to very large scales near and beyond the baryonic acoustic oscillation (BAO) scale. Hence, caution should be taken when using that scale as a cosmic standard ruler: one needs to carefully understand the corresponding biases. The simulation is expected to be an invaluable asset for the interpretation of upcoming deep surveys of the Universe.

• 대한전자공학회논문지TC
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• 제45권12호
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• pp.42-48
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• 2008

차세대 무선 통신 시스템은 멀티밴드/멀티모드 동작이 가능한 RF 송수신기를 필요로 하고 있다. Polar transmitter는 효율적인 switched-mode RF 전력증폭기를 사용함으로써 높은 효율성을 얻을 수 있기 때문에 EDGE (Enhanced Data Rates for GSM Evolution), WCDMA (Wideband Code Division Multiple Access) 및 WLAN (Wireless Local Area Network)과 같이 고속의 데이터 전송율을 지원하는 시스템에 적합한 것으로 알려져 있다. 본 논문에서는 수신단의 구조에 변화를 주지 않으며 또한 추가적인 정보의 전송이 필요 없이 기존 수신기를 그대로 사용할 수 있는 PAPR (Peak-to-Average Power Ratio) 감소기법을 OFDM (Orthogonal Frequency Division Multiplexing) polar transmitter에 적용하여 그 성능을 평가하였다. 이 방법은 polar 변조된 신호에 대하여 피크 윈도잉을 사용한 것으로 다양한 윈도우 형태와 길이를 적용하여 비트오율 (Bit Error rate; BER)과 오차 벡터 크기 (Error Vector Magnitude; EVM)를 측정하였다. 모의실험 결과, 제안된 기법은 효율적인 PAPR 감소와 더불어 클리핑으로 인한 대역의 왜곡 (out-of-band distortion)이 감소함을 관측하였다.

• 한국수자원학회논문집
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• 제31권3호
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• pp.317-326
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• 1998

시계열자료의 분해능력이 뛰어난 wavelet 변환을 사용하여 물소비특성을 분석하였다. Wavelet 변환의 기저함수로는 물수요량의 경우 Coiflets5 함수, 기온측정치의 경우 Coiflets3 함수를 사용하였으며 해석결과 212 scale에서 목표된 장기간에 걸친 변화추이는 hyperbolic tangent 함수의 형태로 전기간에 걸처 꾸준한 증가세를 보였다. 또한 절기혹은 경기주기와 밀접한 관련이 있을 것으로 생각되는 추가수요가 6월과 12월말을 정점으로 발생하였으며 이 추가 수요량은 하절기의 경우 $1,700\;\textrm{cm}^3/hr$, 동절기의 경우 $500\;\textrm{cm}^3/hr$ 정도인 것으로 관측되었다. 정수장 생산량 시계열자료에 내재한 주기성분은 주기가 각각 3.13day, 33.33 hr, 23.98hr와 12hr인 것으로 규명되었다. 진폭은 주기가 23,98hr인 성분이 가장 큰 것으로 밝혀졌으며 2i[i = 1,2,…12] scale에서 목도된 단주기성분들은 Gaussian PDF를 따르는 것이 확인되엇다. 잔차성분의 상호독립성, 자색파여부와 FPE의 최소화를 기준으로 할 경우 물수요량의 최적예측모형으로는 기온을 입력자료로한 다원 AR[32, 16, 23]과 다원 ARM [20, 16, 10, 23]인 것으로 판단된다.

• Wind and Structures
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• 제30권4호
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• pp.433-450
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• 2020

The strong turbulence characteristic of typhoon not only will significantly change flow field characteristics surrounding the large-scale wind turbine and aerodynamic force distribution on surface, but also may cause morphological evolution of coast dune and thereby form sand storms. A 5MW horizontal-axis wind turbine in a wind power plant of southeastern coastal areas in China was chosen to investigate the distribution law of additional loads caused by wind-sand coupling movement of coast dune at landing of strong typhoons. Firstly, a mesoscale Weather Research and Forecasting (WRF) mode was introduced in for high spatial resolution simulation of typhoon "Megi". Wind speed profile on the boundary layer of typhoon was gained through fitting based on nonlinear least squares and then it was integrated into the user-defined function (UDF) as an entry condition of small-scaled CFD numerical simulation. On this basis, a synchronous iterative modeling of wind field and sand particle combination was carried out by using a continuous phase and discrete phase. Influencing laws of typhoon and normal wind on moving characteristics of sand particles, equivalent pressure distribution mode of structural surface and characteristics of lift resistance coefficient were compared. Results demonstrated that: Compared with normal wind, mesoscale typhoon intensifies the 3D aerodynamic distribution mode on structural surface of wind turbine significantly. Different from wind loads, sand loads mainly impact on 30° ranges at two sides of the lower windward region on the tower. The ratio between sand loads and wind load reaches 3.937% and the maximum sand pressure coefficient is 0.09. The coupling impact effect of strong typhoon and large sand particles is more significant, in which the resistance coefficient of tower is increased by 9.80% to the maximum extent. The maximum resistance coefficient in typhoon field is 13.79% higher than that in the normal wind field.

• 한국항공우주학회지
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• 제41권1호
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• pp.40-47
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• 2013

하이브리드 로켓은 고체로켓과 매우 흡사한 내부유동 특성을 가지고 있으므로 와류흘림(vortex shedding)은 하이브리드 로켓에서도 연소안정성에 영향을 미치는 중요한 인자로 판단된다. 본 연구에서는 예연소실에서 와류를 발생시켜 연료 표면와류와의 간섭과 연소특성 변화를 관찰하였다. 기본 형상과 디스크를 장착한 실험 결과, 5개의 주파수 특성이 관찰되었으며 이들은 각각 추진제의 열적지연에 의한 주파수, 디스크, 연료 단면, 후연소실 단면 변화에 의한 와류흘림과 관련된 주파수임을 확인하였다. 특히 디스크 1과 3의 결과를 비교해 보면 디스크 위치에 따라 변화하는 와류흘림이 연소실의 특정 주파수 특성과 상호 간섭하여 공진이 발생하기도 하지만, 또 다른 경우에는 어떠한 간섭도 일어나지 않는 것을 확인하였다. 이러한 선택적 공진현상은 하이브리드 로켓의 비선형 연소안정성 발생을 설명할 수 있는 중요한 메카니즘으로 판단된다.

• 한국항공우주학회지
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• 제35권9호
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• pp.799-804
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• 2007

액체추진제 추력기 연소실의 인젝터로부터 발생하는 분무 거동을 파악하기 위하여 광학계측 기법을 사용한다. 실험에 사용된 인젝터는 지름이 0.406 mm이며 중심축으로부터 30 의 경사각을 이루는 8 개의 노즐 구멍으로 구성된다. 분무생성의 초기조건과 분무발달에 따른 미립화 과정을 분석하기 위해, 이중모드 위상도플러속도계(DPDA)로 측정된 액적의 속도 및 입경 등의 변이 거동을 제시하고 Nd:Yag 레이저평면광에 의해 획득된 순간평면이미지와 함께 고찰한다. 분무액적의 초기 분사속도에 근거한 Re 수와 We 수 등의 무차원 변수를 도출하여 인젝터 발생 분무의 미립화 및 난류성질 등에 대한 분무유동 양식의 범주를 결정한다. 이러한 분무분열에 대한 정성적, 정량적 결과는 향후 새로운 추력기 개발에 확실한 설계 기반을 제공할 것이다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 학술대회
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• pp.367-373
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• 2008

Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년 추계학술대회논문집
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• pp.367-373
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• 2008

Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.