Department News
Computational Fluid Dynamics Simulation of Shock-Wave Turbulent Boundary Layer I
Seminar Date
2004-09-23
Author
지국현
Date
2004-09-23
Views
1842
1. 제 목 : Computational Fluid Dynamics Simulation of Shock-Wave Turbulent Boundary Layer Interaction
2. 연 사 : Professor Doyle D. Knight (Rutgers - The State University of New Jersey)
3. 일 시 : 2004년 10월 7일 (목) 13:00 - 14:30
4. 장 소 : 서울대 신공학관(301동) 117호 세미나실
5. 내 용 : Design of high performance supersonic and hypersonic air vehicles requires accurate simulation methods for prediction of aerothermodynamic loads including mean and root-mean-square fluctuating surface pressure, skin friction and heat transfer. Shock wave-turbulent boundary layer interactions can significantly affect aerothermodynamic load, and therefore accurate methods for their prediction are needed. Recently, an evaluation of Computational Fluid Dynamics (CFD) capability for prediction of shock wave turbulent boundary layer interaction was performed under the auspices of NATO RTO Working Group 10. Five different flow configurations were examined by an international collboration of researchers. Three of the configurations were nominally two-dimensional: a compression corner generated by a ramp, an expansion corner followed by a compression corner, and a planar shock wave impinging on a flat plate. The remaining configurations were three dimensional: a single fin attached normal to flat plate, and two fins attached normal to a flat plate and forming a converging channel. Computational Fluid Dynamics capability for prediction of the detailed flow structure and aerothermodynamic loads was evaluated on the basis of advanced Reynolds-Averaged Navier-Stokes (RANS) and Large Eddy Simulation (LES) models through comparison of the prediction results with experiment. The results of this evaluation will be presented, and directions for future research will be discussed.
6. 약 력 :
B.S. California Institute of Technology, 1971
M.S. Aeronautics, California Institute of Technology, 1972
Ph.D. Aeronautics, California Institute of Technology, 1974
Aerospace Research Laboratory, U.S. Air Force :
Aeronautical Engineer, June 1974 - June 1976
California Institute of Technology :
Research Fellow in Applied Mathematics, June 1976 - August 1977
Rutgers University, Department of Mechanical and Aerospace Engineering :
Assistant Professor, July 1977 - June 1981
Associate Professor, July 1981 - June 1985
Professor I, July 1985 - July 1991 (on leave October 1987 - August 1990)
Professor II, July 1991 - present.
Mary W. Raisler Distinguished Teaching Chair, July 2004 - present.
Associate Fellow, American Institute of Aeronautics and Astronautics, 1985
Faculty Academic Merit Award, Rutgers University, 1979, 1981, 1985, 1987, 1991, 1994, 1995,
1997, 1998, 2002
Pi Tau Sigma Gold Medal, Academic Society of Mechanical Engineers, 1980
7. 문 의 : 기계항공공학부 김종암 교수 (☏ 880-1915)
2. 연 사 : Professor Doyle D. Knight (Rutgers - The State University of New Jersey)
3. 일 시 : 2004년 10월 7일 (목) 13:00 - 14:30
4. 장 소 : 서울대 신공학관(301동) 117호 세미나실
5. 내 용 : Design of high performance supersonic and hypersonic air vehicles requires accurate simulation methods for prediction of aerothermodynamic loads including mean and root-mean-square fluctuating surface pressure, skin friction and heat transfer. Shock wave-turbulent boundary layer interactions can significantly affect aerothermodynamic load, and therefore accurate methods for their prediction are needed. Recently, an evaluation of Computational Fluid Dynamics (CFD) capability for prediction of shock wave turbulent boundary layer interaction was performed under the auspices of NATO RTO Working Group 10. Five different flow configurations were examined by an international collboration of researchers. Three of the configurations were nominally two-dimensional: a compression corner generated by a ramp, an expansion corner followed by a compression corner, and a planar shock wave impinging on a flat plate. The remaining configurations were three dimensional: a single fin attached normal to flat plate, and two fins attached normal to a flat plate and forming a converging channel. Computational Fluid Dynamics capability for prediction of the detailed flow structure and aerothermodynamic loads was evaluated on the basis of advanced Reynolds-Averaged Navier-Stokes (RANS) and Large Eddy Simulation (LES) models through comparison of the prediction results with experiment. The results of this evaluation will be presented, and directions for future research will be discussed.
6. 약 력 :
B.S. California Institute of Technology, 1971
M.S. Aeronautics, California Institute of Technology, 1972
Ph.D. Aeronautics, California Institute of Technology, 1974
Aerospace Research Laboratory, U.S. Air Force :
Aeronautical Engineer, June 1974 - June 1976
California Institute of Technology :
Research Fellow in Applied Mathematics, June 1976 - August 1977
Rutgers University, Department of Mechanical and Aerospace Engineering :
Assistant Professor, July 1977 - June 1981
Associate Professor, July 1981 - June 1985
Professor I, July 1985 - July 1991 (on leave October 1987 - August 1990)
Professor II, July 1991 - present.
Mary W. Raisler Distinguished Teaching Chair, July 2004 - present.
Associate Fellow, American Institute of Aeronautics and Astronautics, 1985
Faculty Academic Merit Award, Rutgers University, 1979, 1981, 1985, 1987, 1991, 1994, 1995,
1997, 1998, 2002
Pi Tau Sigma Gold Medal, Academic Society of Mechanical Engineers, 1980
7. 문 의 : 기계항공공학부 김종암 교수 (☏ 880-1915)
