최소 단어 이상 선택하여야 합니다.
최대 10 단어까지만 선택 가능합니다.
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.
NTIS 바로가기大韓機械學會論文集. Transactions of the Korean Society of Mechanical Engineers. B. B, v.29 no.5 = no.236, 2005년, pp.625 - 632
김광용 (인하대학교 기계공학부) , 장춘만 (한국건설기술연구원 화재설비연구부)
This paper describes the shape optimization of a stator blade in a single-stage transonic axial compressor. The blade optimization has been performed using response surface method and three-dimensional Navier-Stokes analysis. Two shape variables of the stator blade, which are used to define a stacki...
* AI 자동 식별 결과로 적합하지 않은 문장이 있을 수 있으니, 이용에 유의하시기 바랍니다.
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
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
Chima, R. V., 1998, 'Calculation of Tip Clearance Effects in a Transonic Compressor Rotor,' ASME J. Turbomachin., Vol. 120, No. 1, pp. 131-140
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 $k-{\varepsilon}$ Turbulence Model,' ASME J. Turbomachin., Vol. 121, No. 1, pp. 44-58
Chung, J., Shim, J. and Lee, K. D., 2000, '3D Transonic Compressoe Design Optimization with Quasi-3D Flow Physics,' ASME FEDSM00-11075
Denton, J. D. and Xu, L., 2002, 'The Effects of Lean and Sweep On Transonic Fan Performance,' ASME Turbo Expo, GT-2002-30327
Cai, N., Xu, J. and Benaissa, A., 2003, 'Aerodynamic and Aeroacoustic Performance of a Skewed Rotor,' ASME Turbo Expo, GT-2003-38592
Fischer, A., Riess, W. and Seume, J., 2003, 'Performance of Strongly Bowed Stators In a 4-Stage High Speed Compressor,' ASME Turbo Expo, GT-2003-38392
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
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
Kim, C.-T., Kim, J.-H. and Lee, D.-S., 1999, 'Performance Test of a Two Stage Axial Compressor of a Turboshaft Engine for Helicopter,' Proceedings of the KSAS Spring Conference, pp. 327-331
Jameson, A., Pierce, N. A. and Maritnelli, L., 1997, 'Optimum Aerodynamic Design Using the Navier-Stokes Equations,' AIAA 97-0101
Baldwin, B. S. and Lomax, H., 1978, 'Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows,' AIAA 78-0257
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.
*원문 PDF 파일 및 링크정보가 존재하지 않을 경우 KISTI DDS 시스템에서 제공하는 원문복사서비스를 사용할 수 있습니다.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.