• 천문학논총
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• 제30권1호
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• pp.17-29
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• 2015

The IGRINS is a near infrared high resolution spectrograph jointly developed by the Korea Astronomy and Space Science Institute and the University of Texas at Austin. We present design and fabrication of the optomechanical mount for the five mirrors, i.e., an input fold mirror, a slit mirror, a dichroic, and two camera fold mirrors. Based on the structure analysis and the thermal analysis of finite element methods, the optomechanical mount scheme satisfies the mechanical and the thermal design requirements given by the optical tolerance analysis. The performance of the fabricated mirror mounts has been verified through three IGRINS commissioning runs.

• 한국패류학회지
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• 제15권1호
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• pp.21-30
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• 1999

본 연구는 1994년 6월부터 1995년 7월까지 광양만의 조화조간대와 덕산조간대에 서식하는 바지락(Ruditapes philippinarum: Bivalvia)의 성장 양상을 알아보기 위하여 수행되었다. 조화조간대의 평균입도, 표층퇴적물내 유기물 함량, 저서미세조류의 엽록소-a 량은 각각 2.50-4.46 , 4.99-5.11%, 14.53-19.90 $\mu\textrm{g}$ $cm^{-3}$이었으며, 덕산조간대는 각각 0.83-1.66 , 2.22-2.34%, 6.20-6.90 $\mu\textrm{g}$ $cm^{-3}$이었다. 바지락의 각장은 봄-여름에 급격히 증가하였고, 가을로 가면서 서서히 둔화되다가, 겨울에 멈추었다. 반면에 육질부 중량은 봄과 가을에 증가하고, 여름과 겨울에 감소하였다. 상태지수 역시 육질부 중량과 동일한 경향을 보였다. 4개 연령군의 각장의 연성장은 von Bertalanffy 성장모델에 잘 적용되었고, 중량은 Gompertz 성장모델에 잘 적용되었다. 초기 각장 성장률 w, 최대 각장 성장률 AGR$_{max}$는 조화조간대가 덕산조간대보다 높았으며, 동일 조간대내에서는 하부조간대가 상부조간대보다 성장률이 높았다. 즉 개체군 서식밀도가 높은 조화조간대에서 이용가능한 잠재적 먹이량, 서식공간에 대한 경쟁이 심하여 개체 성장률이 낮았다.

• 한국지구과학회지
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• 제40권4호
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• pp.353-381
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• 2019

The general world model for homogeneous and isotropic universe has been proposed. For this purpose, we introduce a global and fiducial system of reference (world reference frame) constructed on a (4+1)-dimensional space-time, and assume that the universe is spatially a 3-dimensional hypersurface embedded in the 4-dimensional space. The simultaneity for the entire universe has been specified by the global time coordinate. We define the line element as the separation between two neighboring events on the expanding universe that are distinct in space and time, as viewed in the world reference frame. The information that determines the kinematics of the geometry of the universe such as size and expansion rate has been included in the new metric. The Einstein's field equations with the new metric imply that closed, flat, and open universes are filled with positive, zero, and negative energy, respectively. The curvature of the universe is determined by the sign of mean energy density. We have demonstrated that the flat universe is empty and stationary, equivalent to the Minkowski space-time, and that the universe with positive energy density is always spatially closed and finite. In the closed universe, the proper time of a comoving observer does not elapse uniformly as judged in the world reference frame, in which both cosmic expansion and time-varying light speeds cannot exceed the limiting speed of the special relativity. We have also reconstructed cosmic evolution histories of the closed world models that are consistent with recent astronomical observations, and derived useful formulas such as energy-momentum relation of particles, redshift, total energy in the universe, cosmic distance and time scales, and so forth. The notable feature of the spatially closed universe is that the universe started from a non-singular point in the sense that physical quantities have finite values at the initial time as judged in the world reference frame. It has also been shown that the inflation with positive acceleration at the earliest epoch is improbable.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2011년도 한국우주과학회보 제20권1호
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• pp.30.4-31
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• 2011

The Korea Astronomy and Space Science Institute (KASI) and the Department of Astronomy at the University of Texas at Austin (UT) are developing a near infrared wide-band high resolution spectrograph, IGRINS (Immersion Grating Infrared Spectrograph). The white-pupil design of the instrument optics uses 7 cryogenic mirrors including 3 aspherical off-axis collimators and 4 flat fold mirrors. Two of the 3 collimators are H- and K-band pupil transfer mirrors and they are designed as compensators for the system alignment in each channel. Therefore, their mount design will be one of the most sensitive parts in the IGRINS optomechanical system. The design work will include the computer-aided 3D modeling and finite element analysis (FEA) to optimize the structural stability of the mount models. The mount body will also include a tip-tilt and translation adjustment mechanism to be used as the alignment compensators.

• 한국항공우주학회지
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• 제32권8호
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• pp.12-19
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• 2004

미소평판 주위의 저속 기체유동장이 기체분자운동론에 근거한 방법으로 조사되었다. 모델충돌적분항으로 단순화된 볼츠만방정식을 Discrete Ordinate 방법과 결합된 유한차분법으로 수치해석 하여 길이가 $20{\mu}m$인 5% 평판 주위의 유동장을 계산하였다. 계산결과가 Information Preservation 방법 및 미끄럼 경계조건을 이용한 연속체 방법에 의한 결과와 비교되었다. 세 가지 서로 다른 방법에 의한 계산결과가 기본적으로 유사한 유동형태를 예측하였으나, 세부적인 변에서는 본 방법의 결과가 다른 두 방법의 결과보다 더 정확함을 보였다.

• 한국항공우주학회지
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• 제30권5호
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• pp.56-61
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• 2002

평판 날개의 플러터에 대한 실험적 연구가 수행되었으며, 여러 가지 플러터 해석 방법들을 실험결과와 비교함으로써 검증하였다. 플러터 실험을 위한 날개 모델과 장치들이 아음속 풍동에 설치되었다. 시스템 식렬법을 이용하여 풍동 실험 데이터로부터 플러터 속도를 예측하였다. 날개 모델의 플러터 해석을 위해 MSC/NASTRAN, V-g방법, 근궤적법이 사용되었다. 해석으로 구한 플러터 속도와 실험으로부터 추정된 플러터 속도를 비교하였으며, 그 결과 잘 일치하였다. 본 연구의 날개 모델이 플러터 해석의 벤치마크 모델로 사용될 수 있을 것이다.

• International Journal of Aeronautical and Space Sciences
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• 제16권3호
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• pp.325-338
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• 2015

Experimental and numerical investigations were conducted to identify the wake characteristics downstream of two vane-type vortex generators over laminar flat plate boundary layer. Experimental study was carried out by using the stereoscopic particle image velocimetry. To describe the flow field around the vortex generator in detail, numerical study was performed. We considered two different planform shapes of vortex generator: triangular and rectangular shape. The height of the generator was chosen to be about the boundary layer thickness at the position of its installation. Two different lengths of the generator were chosen: two and five times the height. Wake measurements were carried out at three angles of attack for each configuration. Wake characteristics for each case such as overall vortical structure, vorticity distribution, and location of vortex center with downstream distance were obtained from the PIV data. Wake characteristics, as expected, were found to vary strongly with the geometry and angle of attack so that no general tendency could be deduced. Causes of this irregular tendency were explained by using the results of the numerical simulation.

• 한국항공우주학회지
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• 제34권3호
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• pp.14-21
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• 2006

직사각형 평판날개의 날개짓과 비틀림 운동을 해석하기 위하여 비정상 와류격자법(VLM)을 이용하였다. 단순 상하 및 피칭 운동하는 날개에 대한 해석결과를 실험 및 다른 수치해석 결과들과 비교하여 복잡한 날개짓 비행을 모사하는데 본 방법을 사용할 수 있음을 보였다. 날개짓 각 진폭이 $20^{\circ}$인 경우에 여러 가지 비틀림 각과 무차원 주파수 변화에 대하여 직사각형 평판 날개의 양력, 추력 및 추진효율을 계산하였다. 계산 결과를 분석하여 주기적으로 변하는 비틀림이 날개짓 날개의 공력 특성에 미치는 영향을 살펴보았다.

• International Journal of Aeronautical and Space Sciences
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• 제14권3호
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• pp.229-236
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• 2013

This paper presents the experimental investigation of a biplane micro air vehicle. The effects of geometric parameters, gap, stagger, and decalage angle are investigated at low Reynolds number (~150,000) in a low-speed wind tunnel. A rigid flat plate with an aspect ratio of one and square planform shape is used to evaluate all three geometric parameters. The side dimension of the single flat plate is 0.15 m. The goal is to find an optimal biplane configuration that should exceed monoplane performance by generating high lift and flying as slow as possible, in order to capture high-quality visual recordings. This configuration will directly help to fly at a lower velocity and to make tighter turns that are advantageous in restricted environments. The results show that the aerodynamic performance of the biplane MAV is significantly enhanced through the combination of gap and stagger effects. A performance comparison demonstrates the superiority of the optimal biplane configuration compared to a monoplane in cruise and glide phases. Moreover, no significant compromise is found for the range, endurance, and climb performance.

• Advances in aircraft and spacecraft science
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• 제6권3호
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• pp.225-238
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• 2019

A spike attached to a blunt nosed body significantly alters its flow field and influences the aerodynamic coefficients at hypersonic speed. The basic body is an axisymmetric, with a hemisphere nose followed by a cylindrical portion. Five different types of spikes, namely, conical aerospike, hemisphere aerospike, flat-face aerospike, hemisphere aerodisk and flat-face aerodisk are attached to the basic body in order to assess the aerodynamic characteristic. The spiked blunt body without the aerospike or aerodisk has been set to be a basic model. The coefficients of drag, lift and pitching moment were measured with and without blunt spike body for the length-to-diameter ratio (L/D) of 0.5, 1.0, 1.5 and 2.0, at Mach 6 and angle of attack up to 8 degrees using a strain gauge balance. The measured forces and moment data are employed to determine the relative performance of the aerodynamic with respect to the basic model. A maximum of 77 percent drag reduction was achieved with hemisphere aerospike of L/D = 2.0. The comparison of aerodynamic coefficients between the basic model and the spiked blunt body reveals that the aerodynamic drag and pitching moment coefficients decrease with increasing the L/D ratio and angle of attack but the lift coefficient has increasing characteristics.