• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2007년도 추계 학술대회논문집
• /
• pp.60-66
• /
• 2007

Separation control has been performed using synthetic jets on airfoil at high angle of attack. Computed results demonstrated that stall characteristics and control surface performance could be substantially improved by resizing separation vortices. It was observed that the actual flow control mechanism and flow structure is fundamentally different depending on the range of synthetic jet frequency. For low frequency range, small vortices due to synthetic jet penetrated to the large leading edge separation vortex, and as a result, the size of the leading edge vortex was remarkably reduced. For high frequency range, however, small vortex did not grow up enough to penetrate into the leading edge separation vortex. Instead, synthetic jet firmly attached the local flow and influenced the circulation of the virtual airfoil shape which is the combined shape of the main airfoil with the separation vortex. Theses results show the characteristic of unsteady flow of single synthetic jet. Beside, we researched on multi-array synthetic jet to obtain applicable synthetic jet velocity. Multi-location synthetic jet is proposed to eliminate small vortex on suction surface of airfoil. With the results, we concluded that the flow around airfoil is stable by high frequency synthetic jet with elimination of small vortex and confirmation of stable flow. Moreover, performance of multi-array/multi-location synthetic jet can be improved by changing phase angle of multi-location synthetic jet.

• International Journal of Aeronautical and Space Sciences
• /
• 제11권4호
• /
• pp.345-350
• /
• 2010

The repetitive vibrating action of an aerodynamic load causes an external fuel tank's horizontal fin to experience a shorter life cycle than its originally predicted one. Store separation analysis is needed to redesign the fin of an external fuel tank. In this research, free-drop tests were conducted using 15% scaled models in a subsonic wind tunnel in order to analyze the store separation characteristics of an external fuel tank. The store separation trajectory based on grid tests was also obtained to verify the results of the free-drop tests. The results acquired from the free-drop tests correlated well with the grid tests in regards to the trajectories and behavior of the stores separated from the aircraft. This agreement was especially noted in the early stages of the store separation.

• International Journal of Aeronautical and Space Sciences
• /
• 제2권2호
• /
• pp.1-18
• /
• 2001

A numerical technique for simulating the separation dynamics of strap-on boosters jettisoned in the dense atmosphere is presented. Six degree of freedom rigid body equations of motion are integrated into the three-dimensional unsteady Navier-Stokes solution procedure to determine the dynamic motions of strap-ons. An automated Chimera overlaid grid technique is introduced to achieve maximum efficiency for multi-body dynamic motion and a domain division technique is implemented in order to reduce the computational cost required to find interpolation points in the Chimera grids. The flow solver is validated by comparing the computed results around the Titan IV launch vehicle with experimental data. The complete analysis process is then applied to the. H-II launch vehicle, the central rocket in japans space program, the CZ-3C launch vehicle developed in China and the KSR-III, a three-stage sounding rocket being developed in Korea. From the analyses, separation trajectories of strap-on boosters are predicted and aerodynamic characteristics around the vehicles at every time interval are examined. In addition, separation-impulse devices generally introduced for safe separation of strap-ons are properly modeled in the present paper and the jettisoning force requirements are examined quantitatively.

• 한국항공우주학회지
• /
• 제34권3호
• /
• pp.37-43
• /
• 2006

접합방법이 다른 6가지 종류의 복합재 보강패널을 제작하고 압축시험을 수행하였다. 모든 패널은 좌굴 및 좌굴 후 거동에서 스킨과 보강재의 분리 파손이 발생하기 전까지는 비슷한 거동 특성을 나타내었다. 분리 파손은 스킨 좌굴 지점과 인접한 보강재 플랜지에서 발생하였으며 분리 파손의 발생 하중, 분리 파손 진전 특성 및 최종 파손 하중은 스킨과 보강재의 접합방법 및 보강재 형상에 따라 다르게 나타났다. 스킨과 보강재의 분리 파손이 일찍 발생하고 크게 전파될수록 보강 패널의 최종 파손 강도 및 구조 효율이 더 많이 저하되었다.

• 한국추진공학회지
• /
• 제22권4호
• /
• pp.91-98
• /
• 2018

본 연구에서는 중첩된 두 비행물체에서 단분리 시 일어나는 주위 유동장 분석에 초점을 맞춰 해석을 수행하였다. 수치 해석을 위하여 정지된 비행체에서 분리되는 실린더 형태의 부스터를 중첩격자를 이용하여 모델링 하였으며 상용해석코드인 $CFD-FASTRAN^{TM}$을 사용하여 계산하였다. 실제 현상을 모사하기 위해서는 부스터에 대한 스프링 반발력, 중력, 상대 속도 등의 고려가 필수적인 요소였다. 연구결과, 부스터의 분리 시간은 비행 마하수와 받음각이 증가함에 따라 감소하는 것을 확인할 수 있었으며, 현재까지의 결과를 종합하여 볼 때 본 연구에서 수행한 모델링과 경계조건 등의 구성이 비행시험의 안전한 부스터 분리와 이후 시퀀스를 예측하는데 많은 도움을 줄 것으로 판단된다.

• 공업화학
• /
• 제10권2호
• /
• pp.319-323
• /
• 1999

비대칭 폴리에테르이미드막을 상전이 방법으로 제조하였고, 표면층 개질에서 NaOH 농도의 영향과 그에 따른 물/이소프로판올 혼합물 투과증발 분리에 대하여 연구하였다. 실험결과, 개질 용액의 농도가 증가할수록 폴리에테르이미드의 이미드 그룹이 가수분해에 의해서 쉽게 폴리아믹산 구조로 변하여 치밀층의 두께가 증가하였다. 따라서 사용된 NaOH 농도가 증가할수록 전반적인 투과도는 감소하였고, 선택도는 증가하였다. 그러나 NaOH 용액의 농도가 너무 높은 경우, 선택도가 오히려 감소하고 투과도는 증가되었다. 이러한 결과로부터, 비대칭 폴리에테르이미드막의 투과거동이 NaOH 농도에 크게 의존한다는 것을 알 수 있었다. 또한, NaOH로부터 개질된 막들의 투과증발 운전온도가 증가할수록 투과도와 선택도가 모두 증가되었다.

• 한국자동차공학회논문집
• /
• 제16권3호
• /
• pp.172-178
• /
• 2008

An object of this study is to confirm performance characteristics of the vortex tube apparatus for substitution of the intercooler in a common-rail diesel engine. The turbo pressure, the intake air flow rate and the ${\Delta}T_c$ decrease ratio of the intercooler were measured in a experimental engine. The vortex tube apparatus was made after confirmation of the geometric phenomena in fundamental experiments. To investigate energy separation characteristics of the vortex tube, the measured turbo pressure was applied to the vortex tube inlet and the ${\Delta}T_c$ decrease ratio was compared with one of the intercooler in the cold air mass flow ratio similar to the intake air flow rate of the experimental engine. From the results, we found that the energy separation ratio is increased according to of the inlet pressure and the ${\Delta}T_c$ decrease ratio of the vortex tube apparatus is higher than one of the intercooler at low engine speed and engine load of medium and low.

• 한국수소및신에너지학회논문집
• /
• 제22권1호
• /
• pp.69-76
• /
• 2011

PEMFC (polymer electrolyte membrane fuel cell) is device that generates electricity from hydrogen. It is one of the subjects related to renewable energy and various research has been conducted on the PEMFC. PEMFC has low operating temperature and high efficiency among fuel cells, and is given attention as means for automobile and domestic use. Analysis of flow field pattern in supplying hydrogen and oxygen is part of the research to increase PEMFC efficiency. In this study, separation plate currently used in PEMFC is transformed to wave shape and mass transfer characteristics in the channel is examined through numerical and experimental analysis. Wave shape separation plate yielded 18% increase of efficiency compared to separation plate used in normal channel. And improvements in mass transfer characteristics were verified.

• 대한조선학회논문집
• /
• 제44권3호
• /
• pp.228-237
• /
• 2007

The flow characteristics around a horn-type rudder behind an operating propeller of a high-speed large container carrier are studied through a numerical method in fully wetted and cavitating flow conditions. The computations are carried out in a small scale ratio of 10.00(gap space=5mm) to consider the gap effects. The Reynolds averaged Navier-Stokes equation for a mixed fluid and vapor transport equation applying cavitation model are solved. The axisymmetry body-force distribution technique is utilized to simulate the flow behind an operating propeller. The gap flow, the three-dimensional flow separation, and the cavitation are the flow characteristics of a horn-type rudder. The pattern of three-dimensional flow separation is analyzed utilizing a topological rule. The various cavity positions predicted by CFD were shown to be very similar to rudder erosion positions in real ship rudder. The effect of a preventing cavitation device, a horizontal guide plate, is also investigated.

• 한국수소및신에너지학회논문집
• /
• 제17권2호
• /
• pp.141-148
• /
• 2006

This study was carried out to analyze the microstructure characteristics of electrolyte membrane through XRD, SEM and AC impedance measurement for using in high temperature steam electrolysis(HTE). It was investigated that thermal stability and electric characteristics by sintering condition using dry and wet process, and confirmed growth of particle and density change by sintering temperature. The sintering temperature and behavior had an effect on the relative density of the ceramic and the average grain size. The more amount of dispersant in organic compound increase, the more the density increased. But the binder was shown opposite phenomenon. It was analyzed that electrolyte resistance and electrical characteristics using AC impedance. The electrical properties of YSZ grain boundary changed with the sintering temperature.