1 |
Jang, C.-M. and Kim, K.-Y., 2005, 'Shape Optimization of a Stator Blade in a Single-Stage Transonic Axial Compressor,' Trans. of the KSME, Series B, Vol. 29, No. 5, pp. 625-632
과학기술학회마을
DOI
|
2 |
Box, M. J. and Draper, N. R., 1971, 'Fractional Designs, the Criterion, and Some Related Matters,' Technometrics, Vol. 13, No. 4, pp. 731-742
DOI
|
3 |
Guinta, A. A., 1997, 'Aircraft Multidisciplinary 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
|
4 |
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 Paper No. 81-1259
|
5 |
Vad, J., Kwedikha, A. R. A. and Jaberg, H., 2004, 'Influence of Blade Sweep on the Energetic Behavior of Axial Flow Turbomachinery Rotors at Design Flow Rate,' ASME Turbo Expo, GT-2004-53544
|
6 |
Baldwin, B. S. and Lomax, H., 1978, 'Thin Layer Approximation and Algebraic Model for Separated Turbulent Flow,' AIAA Paper, No. 78-257
|
7 |
Ahn, C.-S. and Kim, K.-Y., 2003, 'Aerodynamic Design Optimization of A Compressor Rotor with Navier- Stokes Analysis,' Proceedings of the Institution of Mechanical Engineers, Part A-J. Power and Energy, Vol. 217, No. 2, pp. 179-184
DOI
ScienceOn
|
8 |
Ko, W.-S., Kim, K.-Y. and Ko, S.-H., 2003, 'Aerodynamic Design Optimization of A Transonic Axial Compressor Rotor with Readjustment of A Design Point,' Proceedings of the KFMA Annual Meeting, pp. 639-645
과학기술학회마을
|
9 |
Chima, R. V., 1998, 'Calculation of Tip Clearance Effects in a Transonic Compressor Rotor,' ASME J. Turbomachinery, Vol. 120, No. 1, pp. 131-140
DOI
ScienceOn
|
10 |
Reid, L. and 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
|
11 |
Chima, R. V. and Yokota, J. W., 1998, 'Numerical Analysis of Three-Dimensional Viscous Internal Flows,' NASA TM-100878, pp. 1-10
|
12 |
Hah, C., Rabe, D. C. and Wadia A. R., 2004, 'Role of Tip Leakage Vortices and Passage Shock in Stall Inception in a Sweep Transonic Compressor Rotor,' ASME GT2004-53867
|
13 |
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
|
14 |
Watanabe, H. and Zangeneh, M., 2003, 'Design of the Blade Geometry of Swept Transonic Fans by 3D Inverse Design,' ASME Turbo Expo, GT-2003-38770
|
15 |
Denton, J. D. and Xu, L., 2002, 'The Effects of Lean and Sweep on Transonic Fan Performance,' ASME Turbo Expo, GT-2002- 30327
|
16 |
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
|
17 |
Hah, C. and Loellbach, J., 1999, 'Development of Hub Corner Stall and Its Influence on the Performance of Axial Compressor Blade Rows,' ASME J. Turbomachin., Vol. 121, No.1, pp. 67-77
DOI
|
18 |
Madsen, J.I., Shyy, W. and Haftka, R.T., 2000, 'Response Surface Techniques for Diffuser Shape Optimization,' AIAA Journal, Vol. 38, pp. 1512-1518
|