Journal of Ocean Engineering and Technology (한국해양공학회지)

Korean Society of Ocean Engineers (한국해양공학회)
권호 표지

Comparative Study on Numerical Analysis Methods on the 2D Ground Effect

2차원 지면효과에 대한 수치해석 기법 비교 연구

  • Kim, Yoon-Sik (Marine Transportation and Safety Research Department, MOERI/KORDI) ;
  • Shin, Myung-Soo (Marine Transportation and Safety Research Department, MOERI/KORDI) ;
  • Cho, Yong-Jin (Marine Transportation and Safety Research Department, MOERI/KORDI)
  • 김윤식 (한국해양연구원 해양시스템안전연구소 해양운전안전연구본부) ;
  • 신명수 (한국해양연구원 해양시스템안전연구소 해양운전안전연구본부) ;
  • 조용진 (한국해양연구원 해양시스템안전연구소 해양운전안전연구본부)
  • Published : 2007.06.29
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Abstract

A comparative study on the turbulent flaw simulation and the potential flaw analysis has been performed. A law Mach number preconditioned Navier-Stokes solver, using the multi-block grid method and a panel method based on the velocity potential, have been developed and validated by comparison to the experimental data. The present numerical analysis methods are applied to the ground effect problem around the NACA 4412 airfoil. It has been confirmed that the potential flaw analysis on the ground effect, using the image method, is consistent, to some degree, with the viscous calculations for high Reynolds number flows.

Keywords

References

  1. 라승호, 정진덕, 옥호남, 권기정, 조태환, 최인호 (2000). 'WIG 공력특성에 대한 풍동시험', 한국항공우주학회지, 제28권, 제2호, pp 1-9
  2. 박일룡, 전호환 (1998). '3차원 표면효과익의 정상 및 비정상 성능해석', 대한조선학회논문집, 제35권, 제3호, pp 14-25
  3. 신명수, 김윤식, 이경중, 강국진, 박영하, 이영연 (2006). '소형 위그선 개념 설계', 대한조선학회논문집, 제43권, 제1호, pp 134-146 https://doi.org/10.3744/SNAK.2006.43.1.134
  4. 이주희, 김병삼, 박경우 (2006). '지면효과를 고려한 WIG선 인형의 공력특성 및 형상최적화', 대한기계학회논문집 B권, 제30권, 제11호, pp 1084-1092 https://doi.org/10.3795/KSME-B.2006.30.11.1084
  5. 전호환, 장용훈, 신명수 (2002). 'CFD에 의한 2차원 지면 효과익 주위의 난류유동계산', 대한조선학회논문집, 제39권, 제3호, pp 28-40
  6. 전호환, 장종희, 백광준 (1999). '해면효과익선의 종방향 안정성에 대한 연구', 대한조선학회논문집, 제36권, 제3호, pp 60-70
  7. 조정현, 김윤제 (2001). '지면효과를 받는 2차원 에어포일 주위유동에 대한 연구', 한국항공우주학회지, 제29권, 제5호, pp 17-24
  8. 조창열, 김양준 (2004). '지면효과익기 날개에 대한 전산 공력 해석', 한국항공우주공학회지, 제32권, 제8호, pp 37-46
  9. Abbott, I.H and von Doenhoff, A. (1959). Theory of Wing Sections-Including a Summary of Airfoil Data, Dover Pub., New York, NY, USA
  10. Barber, T. (2006). 'Aerodynamic Ground Effect: A Case Study of the Integration of CFD and Experiments', Int. J. Vehicle Design, Vol 40, No 4, pp 299-316 https://doi.org/10.1504/IJVD.2006.009068
  11. Bagely, J.A. (1960). 'The Pressure Distribution on Two-Dimensional Wings near the Ground', A.R.C. R.&M. 3238
  12. Barlow, J.B., Rae, W.H. and Pope, A. (1999). Low-Speed Wind Tunnel Testing, 3rd ed., John Wiley & Sons, New York, NY, USA
  13. Carter, A.W. (1961). 'Effect of Ground Proximity on the Aerodynamic Characteristics of Aspect-Ratio-1 Airfoils With and Without End Plates', NASA TN D-970
  14. Delhaye, H. (1997). An Investigation into the Longitudinal Stability of Wing In Ground effect Vehicles, MSc. Thesis, Cranfield Univ., Cranfield
  15. Fach, H., Fisher, H., Kornev, N. and Peterson, U. (2004). 'Wing In Ground(WIG) Craft', Ship Design and Construction, Vol 2, Ch. 48, Lamb, T. ed., SNAME
  16. Fink, M.P. and Lastinger, J.L. (1961). 'Aerodynamic Characteristics of Low-Aspect-Ratio Wings in Close Proximity to the Ground', NASA TN D-926
  17. Gault, D. E. (1957). 'A Correlation of Low-Speed, Airfoil-Section Stalling Characteristics with Reynolds Number and Airfoil Geometry', NACA TN-3963
  18. Hayashi, M. and Endo, E. (1978). 'Measurement of Flow Fields around an Airfoil Section with Separation', Trans. Japan Soc. Aero. Space Sci., Vol 21, No 52, pp 69-75
  19. Hirata, N. and Kodama, Y. (1995). 'Flow Computation for Three-Dimensional Wing in Ground Effect Using Multi-Block Technique', J. of the Society of Naval Architects of Japan, Vol 177, pp 49-57
  20. Jespersen, D., Pulliam, T., and Burning, P. (1997). 'Recent Enhancements to OVERFLOW', AIAA Paper 97-0644
  21. Katz, J., and Plotkin, A. (1991). Low-Speed Aerodynamics: From Wing Theory to Panel Methods, McGraw-Hill, New York, NY, USA
  22. Kim, Y., and Kwon, J.H. (2000). 'KGRID: An Interactive 3D Grid Generator with GUI', 4th ACFD Conf. Proc
  23. Kumar, P.E. (1968). 'An Experimental Investigation into the Aerodynamic Characteristics of a Wing, With and Without Endplates, in Ground Effect', CoA Report Aero No. 201, The College of Aeronautics Cranfield
  24. Lockheed Report 16906 (1964). 'Wind-Tunnel Investigation of Single and Tandem Low-Aspect-Ratio Wings in Ground Effect', Lockheed California Com., USA
  25. Maskalik, A.I., Kolyzaev, B., Zhukov, V., Radovitski, G., Sinitsyn, D., and Zagorulko, L. (2000). Ekranoplans. Peculiarities of the Theory and Design, Sudostroenie, St. Petersburg, Russia
  26. McGhee, R.J., and Beasley, W.D., Somers, D.M. (1977). 'Low-Speed Aerodynamic Characteristics of a 13-Percent- Thick Airfoil Section Designed for General Aviation Applications', NASA TM X-72697
  27. Park, S.H., and Kwon, J.H. (2004). 'Implementation of k-w Turbulence Models in an Implicit Multigrid Method', AlAA J., Vol 42, No 7, pp 1348-1357
  28. Park, S.H., Lee, J.E. and Kwon, J.H. (2006). 'Preconditioned HLLE Method for Flows at All Mach Numbers', AlAA J., Vol 44, No 11, pp 2645-2653
  29. Perkins, C.D. and Hage, R.E. (1949). Airplane Performance: Stability & Control, John Wiley & Sons, Hoboken, NJ, USA
  30. Pulliam, T. H. and Chaussee, D.S. (1981). 'A Diagonal Form of an Implicit Approximate Factorization Algorithm', J. Comp. Phys., Vol 39, pp 347-363 https://doi.org/10.1016/0021-9991(81)90156-X
  31. Roe, P.L. (1981). 'Approximate Riemann Solver, Parameter Vectors and Difference Schemes', J. Comput. Phys., Vol 43, No 2, pp 357-372 https://doi.org/10.1016/0021-9991(81)90128-5
  32. Shin, M.S. (2000). 'Model Test Survey Report of Wing-in-Ground Effect Ship', J. of Ships and Ocean Eng., Vol 29, pp 23-27
  33. Shin, M.S., Yang, C.J., Yang, S.I., and Wang, G.Q. (1999). 'Numerical Simulation of Viscous Flow Around a Three- Dimensional Wing in Ground Effect with Endplates', FAST '99 Conf. proceeding, Seattle, US, pp 593-603
  34. Steinbach, D., and Jacob, K. (1991). 'Some Aerodynamic Aspects of Wings near Ground', Trans. Japan Soc. Aero. Space Sci. Vol 34, No 104, pp 56-70
  35. Thivet, F. (2002). 'Lessons Learned from RANS Simulations of Shock-Wave/Boundary Layer Interactions', AlAA Paper 2002- 0583
  36. Venkateswaran, D.L. and Merkle, C.L. (2003). 'Influence of Stagnation Regions on Preconditioned Solutions at Low Speeds', AlAA Paper 2003-0435
  37. Weiss, J.M. and Smith, W.A. (1995). 'Preconditioning Applied to Variable and Constant Density Flows', AlAA J., Vol 33, No 11, pp 2050-2057
  38. Wilcox, D.C. (1988). 'Reassessment of the Scale-Determining Equation for Advanced Turbulence Models', AlAA J., Vol 26, No 11, pp 1299-1330
  39. Yates, A.H. (1952). 'Notes on the Mean Aerodynamic Chord and the Mean Aerodynamic Centre of a Wing', J. of the Royal Aeron. Soc., 461-474