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초음속 충돌 제트 운동에 대한 k-$\omega$ 난류모델의 적용
김유진,박수형,권장혁,김성인,박승오,이광섭,홍승규,Kim E.,Park S. H.,Kwon J. H.,Kim S. I.,Park S. O.,Lee K. S.,Hong S. G. 한국전산유체공학회 2004 한국전산유체공학회지 Vol.9 No.2
A numerical study of underexpanded jet and impingement on a wall mounted at various distances from the nozzle exit is presented. The 3-dimensional Wavier-Stokes equations and κ-ω turbulence equations are solved. The grids are constructed as overlapped grid systems to examine the distance effect. The DADI method is applied to obtain steady-state solutions. To avoid numerical instability such as the carbuncle phenomena that sometimes accompany approximate Riemann solver, the HLLE+ scheme is employed for the inviscid flux at the cell interfaces. A goal of this work is to apply a number of two-equation turbulence models based on the w equation to the impinging jet problem.
김유진,김상아,윤희림,이진영,전혜빈,박수이,Kim, Yu-jin,Kim, Sang-a,Yun, Hee-rim,Lee, Jin-young,Jeon, Hye-bin,Park, Su-e 한국정보통신학회 2019 한국정보통신학회논문지 Vol.23 No.1
최근 의료 기술의 발달로 제1형 당뇨에 대한 진단율이 높아지면서 당뇨 환아가 증가하고 있다. 이러한 상황에서 환아들에게 당뇨 교육이 필요하지만, 효율적이고 적절한 교육 콘텐츠는 부재한 상황이다. 특히 이러한 교육은 혈당 변화 대처요령과 행동치료에 대한 꾸준하고 반복적인 학습이 필요하다. 따라서 본 연구에서는 10-11세 환아들의 눈높이에 맞춰 주도적으로 학습할 수 있는 에듀테인먼트 콘텐츠를 제안하고자 한다. 효과적인 학습을 위해 주사 실습콘텐츠를 구성하였고 반복적인 학습을 위해 하이브리드방식을 사용하였다. 사용성 테스트를 통해서 이러한 구성이 효과적임을 알 수 있었다. 본 연구는 상대적으로 당뇨 교육을 받기 어려운 지역의 환아들이 쉽게 접근 가능함과 동시에 앞으로 개발될 아동의 눈높이에 맞춘 당뇨 교육 콘텐츠 연구의 기반 연구로써 공헌할 것으로 기대된다. With the recent development of medical technology, the diagnosis rate of type 1 diabetes is increasing and patients are increasing. However, diabetes education content is not aligned with the interest level of children. As a result of the interviews with experts, It was found that the measures of coping with the change of blood sugar and the behavior therapy require steady and repetitive learning. Therefore, this study proposes Edutainment content which can be repeatedly Learned by 10~11year old children. For effective learning, the contents of the laboratory practice were constructed and the hybrid method was used for the repetitive learning. Usability test showed that this configuration is effective. This study is expected to contribute to the study of diabetic education content that is suitable for the children's level of understanding which will be developed easily in the future.
김유진(E. Kim),박수형(S. H. Park),권장혁(J. H. Kwon),김성인(S. I. Kim),박승오(S. O. Park),이광섭(K. S. Lee),홍승규(S. K. Hong) 한국전산유체공학회 2004 한국전산유체공학회 학술대회논문집 Vol.2004 No.-
A numerical study of underexpanded jet and impingement on a wall mounted at various distances from the nozzle exit is presented. The 3-dimensional Navier-Stokes equations and k-ω turbulence equations are solved. The grids are constructed as overlapped grid systems to examine the distance effect. The DADI method is applied to obtain steady-state solutions. To avoid numerical instability such as the carbuncle that sometimes accompany approximate Riemann solver, the HLLE+ scheme is employed for the inviscid flux at the cell interfaces. A goal of this work is to apply a number of two-equation turbulence models based on the ω equation to the impinging jet problem.
김유진(E. Kim),박수형(S.H. Park),권장혁(J.H. Kwon),김성인(S.I. Kim),박승오(S.O. Park),이광섭(K.S. Lee),홍승규(S.K. Hong) 한국전산유체공학회 2004 한국전산유체공학회지 Vol.9 No.2
A numerical study of under expanded jet and impingement on a wall mounted at various distances from the nozzle exit is presented. The 3-dimensional Navier-Stokes equations and k-ω turbulence equations are solved. The grids are constructed as overlapped grid systems to examine the distance effect. The DADI method is applied to obtain steady-state solutions. To avoid numerical instability such as the carbuncle phenomena that sometimes accompany approximate Riemann solver, the HLLE+ scheme is employed for the inviscid flux at the cell interfaces. A goal of this work is to apply a number of two-equation turbulence models based on the ω equation to the impinging jet problem.
헬리콥터로부터 발사된 로켓의 공력 간섭 현상에 대한 수치적 연구
이범석(B.S. Lee),김유진(E.J. Kim),강경태(K.T. Kang),권오준(O.J. Kwon) 한국전산유체공학회 2011 한국전산유체공학회지 Vol.16 No.1
Numerical simulation of air-launched rockets from a helicopter was conducted to investigate the aerodynamic interference between air-launched rocket and helicopter. For this purpose, a three-dimensional inviscid flow solver has been developed based on unstructured meshes. An overset mesh technique was used to describe the relative motion between rocket and rocket launcher. The flow solver was coupled with six degree-of-freedom equation to predict the trajectory of free-flight rockets. For the validation, calculations were made for the impinging jet with inclined plate. The rotor downwash of helicopter was calculated and applied to simulation of air-launched rocket. It is shown that the rotor downwash has non-negligible effect on the air-launched rocket and its plume development.
헬리콥터로부터 발사된 로켓의 초기 안정성에 대한 수치적 연구
이범석(B. S. Lee),김유진(K. T. Kang),강경태(E. J. Kim),권오준(O. J. Kwon) 한국전산유체공학회 2010 한국전산유체공학회 학술대회논문집 Vol.2010 No.11
Numerical simulation of air-launched rockets from a helicopter was conducted to investigate the initial aerodynamic stability and its plume effect. For this purpose, a three-dimensional inviscid flow solver has been developed based on unstructured meshes and an mesh technique was used to describe the relative motion between missile launcher and launched rockets. The flow solver was coupled with six degree-of-freedom equation to predict the trajectory of free-flight rockets. Simulation of air-launched rockets from a helicopter showed that rotor downwash has non-negligible effect on the initial stability of the rockets and its plume development.