• The Bulletin of The Korean Astronomical Society
• /
• v.37 no.1
• /
• pp.60.2-60.2
• /
• 2012

Sco OB1의 핵심성단 NGC 6231를 호주 Siding Spring 천문대 1m 망원경을 사용하여 -40'${\times}$40' 영역을 관측하였다. 측광자료를 바탕으로 성단의 반경, 성간소광 법칙, 나이 및 초기질량함수를 결정하였다. 성단의 반지름은 구성원의 질량에 상관없이 거의 10' ($R{\approx}4.6pc$)으로 동일한 값을 보였다. 전체적으로는 정상적인 성간소광 법칙을 따르지만, 성단의 중심으로 갈수로 큰 $R_V$를 보여주며, 이는 과거에 있었을 것으로 추정되는 초신성의 효과로 추정된다. 질량이 큰 별과 X-선으로 선택된 성단의 전주계열성은 비슷한 평균나이를 보이지만 전주계열성은 훨씬 큰 나이분산을 보였다. 성단전체 초기질량함수의 기울기는 Salpeter 초기질량함수의 기울기와 매우 유사한 ${\Gamma}$=-1.1${\pm}$0.1을 보였으며, 성단 중심거리에 따른 초기질량함수의 기울기는 -1.0${\pm}$0.2에서 -1.8${\pm}$0.5까지 체계적으로 변화를 하였다. 질량이 큰 O형 별의 쌍성비율이 중심거리에 따른 변화를 보이지 않음에 비추어 볼 때, NGC 6231의 질량분리 양상은 역학적 진화의 결과가 아니라 원초적 질량분리현상으로 결론을 내릴 수 있다.

• Journal of the Korean Geographical Society
• /
• v.35 no.4
• /
• pp.503-518
• /
• 2000

분수계는 지형적 실체이며, 지역의 지형 연구 분야에서 자연적 경계로서 설정된다. 분수계는 수계, 산계, 유역등의 지형 요소들과 연관된다. 분수계의 지형 형성과 기능은 경사의 법칙, 구조의 법칙, 그리고 계층의 법칙으로 설명될 수 있다. 분수계는 구조적 형성과정과 기후적 삭박과정을 통하여 변화한다. 지형분수계는 능선분수계, 하천 분수계, 폐쇄 분수계, 세탈 분수계, 문턱 분수계, 세포형 분수계 등으로 유형화 될 수 있다. 지하수 분수계는 대개 지형의 기복을 반영하지만, 지역의 지질구조, 암서, 파쇄대 등으로 인하여 지형 분수계와 일치하지 않을 수 있다. 분수계의 법칙의 예외로서 설명되는 분수계의 일반적 단면은 선형이 아닌 대상 혹은 지대로서 나타난다. 분수계를 물의 흐름을 분리하는 곳으로 볼 때, 지형분수계는 지표면의 고도에 의해서 결정되며, 지하수 분수계는 지형, 지질 구조, 선구 조적 지형 요소들의 배열, 지층의 방향을 고려하여 결정된다.

• Water for future
• /
• v.17 no.4
• /
• pp.269-272
• /
• 1984

우선 홍수유량은 강우가 수문유출계를 통하여 변환된 것이므로, 원리적으로는 유량데이터만으로, 즉 강우데이터 없이도 홍수예측이 가능함을 기술한다. 다음에는 강우유출계의 강한 비선형성은 유량을 수치휠터에 의해 2~3의 성분으로 분리할 때 각성분계부터는 제거되는 것(단, 강우의 분리법칙이 비선형이 된다. "휠터 분리 AR법")에 대하여 기술한다. 제삼으로, 실측유량과 예측유량의 오차가 가장 신뢰도가 높은 정보임을 지적하고, 이 오차를 이요하는 휠터링의 방법으로서 세가지의 고찰법이 있음을 제시한다. 마지막으로 역산강우에 칼만.휠터를 적용하는 방법을 제안하고, 그 방법을 효과적으로 하는 여러 가지 기법을 기술한다. 기법을 기술한다.

• Journal of the Korean Society of Groundwater Environment
• /
• v.4 no.3
• /
• pp.111-115
• /
• 1997

Discrete fracture model has become one of the alternatives for the classical continuum model to simulate the irregular aspects of the fluid flow and the solute transport in fractured rocks. It is based on the assumptions that the discharge in a single fracture is proportional to the cube of the aperture and the fractured rock can be represented by the statistical assemblage of such single fractures. This study is intended to evaluate the effect of the fracture junction on the cubic law. Numerical solution of flow in junction system was obtained by using the Boundary-Fitted Coordinate System (BFCS) method. Results with different intersection angles in crossing fractures show that the geometry of the junction affects the discharge pattern under the same simulation conditions. Therefore, strict numerical and experimental examinations on this subject are required.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.46 no.10
• /
• pp.814-822
• /
• 2018

This paper proposes a guidance law for missiles with control time constraint. Because the proposed guidance law is based on a time-to-go polynomial, it has a generalized form. Also, acceleration of the proposed law converges to zero at the end of the control time, which reduces the sensitivity to the time-to-go estimation error and can increase the flight stability when the separation of the missile appears. A prediction method of the time-to-go is proposed for implementing the proposed law, and the possibility of application to the midcourse and terminal guidance phases is dealt with for exoatmospheric interception. The characteristics and performance of the proposed law are analyzed throughout various simulations.

• Journal of the Korean Society of Hazard Mitigation
• /
• v.8 no.4
• /
• pp.47-52
• /
• 2008

Important factor in designing a breakaway sign support is the velocity change of the impact vehicle. It is measured from the crash test or can be calculated by 3-D Finite Element Analysis. It can also be calculated with relative ease utilizing energy and momentum conservation. In this paper a formula to calculate the velocity change of a car during the time of impact against a small sign is derived utilizing the energy and momentum balance. Using the formula, parametric studies were conducted to find that impact speed, separation force and Breakaway Fracture Energy(BFE) of the posts which represent the degree of fixedness to the foundation are the important factor to vehicle's speed change. It is shown that speed change is larger in the lower speed impact and to the posts with large separation force and BFE.

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.36 no.7
• /
• pp.713-721
• /
• 2012

The finite element simulations of fatigue crack growth are carried out. Using only the mechanical properties usually obtained from the tensile test as input data, we attempted to predict the fatigue crack growth behavior. The critical crack opening displacement is determined by monitoring the change in displacements at the node close to the crack tip. Crack growth is simulated by debonding the crack tip node. The exponent in the Paris law was determined and compared to the published exponent. Plotting with respect to the effective stress intensity factor range yielded more consistent results.

• Journal of the Computational Structural Engineering Institute of Korea
• /
• v.31 no.3
• /
• pp.121-125
• /
• 2018

In this study, finite element analyses of crack propagation along a sinusoidal interface are performed by using cohesive elements. BK law is used for cohesive zone to consider mixed mode traction-separation relation at the crack tip on a sinusoidal interface of a double cantilever beam specimen. The shape of a sinusoidal interface crack and the cohesive strength and the cohesive energies in mixed mode cohesive laws are varied in numerical experiments, and load-displacement curves at the ends of a double cantilever beam specimen are obtained to investigate the crack propagation behavior along a sinusoidal interface.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.33 no.5
• /
• pp.57-64
• /
• 2005

Modern versions of supersonic jet fighter aircraft using digital flight-by-wire flight control system receive aircraft flight condition such as altitude, airspeed and AoA(angle of attack) from IMFP(Integrated Multi-Function Probe). IMFP sensors data have triplex structure using three IMFP sensors. An air data reconfiguration mode is applied to a T-50 flight control law to guarantee the aircraft flight stability when 2 or 3 IMFP sensors data are invalided. In this study, linear analysis and HQS(Handling Quality Simulator) pilot simulation are performed to analyze flight stability when the air data reconfiguration mode is applied to the control law. And we propose an example that the air data reconfiguration mode is applied to the control law due to second failure of IMFP during T-50 flight. It is found that the aircraft flight stability is not affected when the T-50 flight control law is changed to the air data reconfiguration mode.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.32 no.9
• /
• pp.80-87
• /
• 2004

Active control of on-orbit spacecraft jitter is a significant problem for future spacecraft mission requiring stringent pointing performance. Jitter is major disturbance source degrading payload pointing performance. Both passive and active jitter isolation techniques have been studied during the last decade. We present active jitter isolation for a model device in this work. The device provides active control capability by 3 degree-of-freedom control of payload in feedback control strategy. Mathematical modeling of the device is pursued which is naturally used for a baseline controller design. Simulation results are used to validate the designed control law.