DOI QR코드

DOI QR Code

반응면 기법을 이용한 천음속 축류압축기의 삼차원 형상 최적설계

Design Optimization of An Axial-Flow Compressor Rotor Using Response Surface Method

  • 안찬솔 (인하대학교 대학원 기계공학과) ;
  • 김광용 (인하대학교 기계공학부)
  • 발행 : 2003.02.01

초록

Design optimization of a transonic compressor rotor (NASA rotor 37) using response surface method and three-dimensional Navier-Stokes analysis has been carried out in this work. Baldwin-Lomax turbulence model was used in the flow analysis. Three design variables were selected to optimize the stacking line of the blade. Data points for response evaluations were selected by D-optimal design, and linear programming method was used for the optimization on the response surface. As a main result of the optimization, adiabatic efficiency was successfully improved. It is also found that the design process provides reliable design of a turbomachinery blade with reasonable computing time.

키워드

참고문헌

  1. Lakshminarayana, B., 1996, Fluid Dynamics and Heat Transfer of Turbo machinery, John Wiley & Sons, New York
  2. Suder, K. L. and Celestina, K. L, 1994, 'Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor,' ASME paper 94-GT-365
  3. Chima, R. V., 1998, 'Calculation of Tip Clearance Effects in a Transonic Compressor Rotor,' ASME J. Turbomachinery, Vol. 120, No. 1, pp. 131-140 https://doi.org/10.1115/1.2841374
  4. Hah, C. and Loellbach, J., 1999, 'Development of Hub Corner Stall and Its Influence on the Performance of Axial Compressor Blade Rows,' ASME J. Turbomachinery, Vol. 121, No. 1, pp. 67-77 https://doi.org/10.1115/1.2841235
  5. Arima, T., Sonoda, T., Shirotori, M., Tamura, A. and Kikuchi, K., 1999, 'A Numerical Investigation of Transonic Axial Compressor Rotor Flow Using a Low-Reynolds-Number k-Turbulence Model,' ASME J. Turbomachinery, Vol. 121, No. 1, pp. 44-58 https://doi.org/10.1115/1.2841233
  6. Lee, S. Y. and Kim, K. Y., 2000, 'Design Optimization of Axial Flow Compressor Blades with Three-Dimensional Navier-Stokes Solver,' ASME paper 2000-GT-0488
  7. Chung, J., Shim, J., and Lee, K. D., 2000, '3D Transonic Compressoe Design Optimization with Quasi-3D Flow Physics,' ASME FEDSM00-11075
  8. Jameson, A., Pierce, N. A., Maritnelli, L., 1997, 'Optimum Aerodynamic Design Using the Navier-Stokes Equations,' AIAA 97-0101
  9. Myers, R. H., Montgomery, D. C, 1995, 'Response Surface Methodology: Process and Product optimization Using Designed Experiments,' John Wiley & Sons
  10. Shyy, W., Papila, N., Vaidyanathan, R, and Tucker, K., 2001, Progress in Aerospace Science, Vol. 37, pp. 59-118 https://doi.org/10.1016/S0376-0421(01)00002-1
  11. Madsen, J.I., Shyy, W. and Haftka, R.T., 2000, 'Response Surface Techniques for Diffuser Shape Optimization,' AIAA Journal, Vol. 38, pp.1512-1518 https://doi.org/10.2514/2.1160
  12. Sevant, N. E., Bloor, M. I. G., and Wilson, M. J., 2000, 'Areodynamic Design of a Flying Wing Using Response Surface Methodology,' J. Aircraft, Vol. 37, No. 4, pp. 562-569 https://doi.org/10.2514/2.2665
  13. Sobieszczanski-Sobieski, J. and Haftka, R. T., 1996, 'Multi disciplinary Aerospace Design Optimization: Survey of Recent Development,' AIAA 96-0711
  14. Han, W., Wang, Z., Tan, C, Shi, H., and Zhou, M., 1994, 'Effects of Leaning and Curving of Blades With High Turning Angles on the Aerodynamic Characteristics of Turbine Rectangular Cascades,' J. of Turbomachinery, Vol. 116, pp. 417-424 https://doi.org/10.1115/1.2929428
  15. Sasaki, T. and Breugelmans, F., 1998, 'Comparison Sweep and Dihedral Effects on Compressor Cascade Performance,' ASME J. Turbomachinery, Vol. 120, No. 3, pp. 454-464 https://doi.org/10.1115/1.2841738
  16. Beiler, M. G., and Carolus, T. H., 1999, 'Computation and Measurement of the Flow in Axial Flow Fans with Skewed Blades,' ASME Journal of Turbomachinery, Vol. 121, pp. 59-66 https://doi.org/10.1115/1.2841234
  17. Cai, N. and Xu, J. H., 2001, Aerodynamic-Aeroacoustic Performance of Parametric Effects for Skewed-Swept Rotor, ASME paper 2001-GT-0354
  18. Baldwin, B. S. and Lomax, H., 1978, Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows, AIAA 78-0257
  19. Chima, R. V., 1996, 'Application of the k-Turbulence Model to Quasi-Three-Dimensional Turbomachinery Flows,' J. Propulsion Power, Vol. 12, No. 6, pp. 1176-1179 https://doi.org/10.2514/3.24159
  20. Jameson, A., Schmidt, W., and Turkel, E., 1981, Numerical Solutions of the Euler Equation by Finite Volume Methods Using Runge-Kutta Time Stepping Schemes, AIAA 81-1259
  21. Myers, R. H., 1999, 'Response Surface Methodology-Current Status and Future Direction,' Journal of Quality Technology, Vol. 31, No. 1, pp. 30-44
  22. Box, M. J. and Draper, N. R., 1971, 'Fractional Designs, the XTX Criterion, and Some Related Matters,' Technometrics, Vol. 13, No. 4. pp. 731-742 https://doi.org/10.2307/1266950
  23. Venter, G., Haftka, R. T., and Starnes, J. H. Jr., 1996, Construction of Response Surfaces for Design Optimization Applications, AIAA 96-4040-CP
  24. Guinta, A. A., 1997, 'Aircraft Multi-disciplinary Design Optimization Using Design of Experimental Theory and Response Surface Modeling Methods,' Ph. D. Dissertant, Department of Aerospace Engineering, Virginia Polytechnic Institute and State University, Blacksburg, VA
  25. Reid, L., Moore, R. D., 1978, 'Design and Overall Performance of Four Highly-Loaded, High-Speed Inlet Stages for an Advanced, High-Pressure-Ratio Core Compressor,' NASA TP-1337
  26. Hobbs, D. E., Weingold, H. D., 1984, 'Development of Controlled Diffusion Airfoils for Multistage Compressor Application,' J. of Engineering for Gas Turbines and Power, Vol. 106, pp. 271-278 https://doi.org/10.1115/1.3239559
  27. Damle, S., Dang, T., Stringham, J., Razinsky, E., 1999, 'Practical Use of Three-Dimensional Inverse Method for Compressor Blade Design,' J. of Turbomachinery, Vol. 121, pp. 321-325 https://doi.org/10.1115/1.2841317

피인용 문헌

  1. Flow Network Analysis for the Flow Control of a Main Cooling Water System in the HANARO Fuel Test Loop vol.12, pp.5, 2009, https://doi.org/10.5293/KFMA.2009.12.5.007
  2. vol.12, pp.5, 2009, https://doi.org/10.5293/KFMA.2009.12.5.072
  3. Multidisciplinary Design Optimization of 3-Stage Axial Compressorusing Artificial Neural Net vol.13, pp.6, 2010, https://doi.org/10.5293/KFMA.2010.13.6.019