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Effective Performance Prediction of Axial Flow Compressors Using a Modified Stage-Stacking Method
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 Title & Authors
Effective Performance Prediction of Axial Flow Compressors Using a Modified Stage-Stacking Method
Song, Tae-Won; Kim, Jae-Hwan; Kim, Tong-Seop; Ro, Sung-Tack;
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In this work, a modified stage-stacking method for the performance prediction of multi-stage axial flow compressors is proposed. The method is based on a simultaneous calculation of all interstage variables (temperature, pressure, flow velocity) instead of the conventional sequential stage-by-stage scheme. The method is also very useful in simulating the effect of changing angles of the inlet guide vane and stator vanes on the compressor operating characteristics. Generalized stage performance curves are used in presenting the performance characteristics of each stage. General assumptions enable determination of flow path data and stage design performance. Performance of various real compressors is predicted and comparison between prediction and field data validates the usefulness of the present method.
Multi-Stage Axial Flow Compressor;Stage-Stacking;Perform-ance;Design;Off-Design;Fixed Geometry;Variable Geometry;Simultaneous Calculation;
 Cited by
가스터빈의 설계 성능과 부분부하 성능 사이의 상관관계 분석,김동섭;

대한기계학회논문집B, 2002. vol.26. 8, pp.1164-1171 crossref(new window)
해석적 방법을 이용한 가스터빈 축류 압축기의 파울링 현상 해석,송태원;김동섭;김재환;손정락;노승탁;

대한기계학회논문집B, 2001. vol.25. 12, pp.1721-1729 crossref(new window)
Stone, A., 1958, 'Effects of Stage Characteristics and Matching on Axial Flow Compressor Performance,' Trans. ASME, Vol. 80, pp. 1273-1293

Doyle, M. D., and Dixon, S. L., 1962, 'The Stacking of Compressor Stage Characteristics to Give an Overall Compressor Performance Map,' Aeronautical Quarterly, Nov. pp. 349-367

Robbins, W. H., and Dugan, J. F., 1965, ' Prediction of Off-Design Performance of Multi-stage Compressors,' NASA SP-36, pp. 297-310

Muir, D. E., Saravanamuttoo, H. I. H., and Marshall D. J., 1989, 'Health Monitoring of Variable Geometry Gas Turbines for the Canadian Navy,' ASME Journal of Engineering for Gas turbines and Power, Vol. 111, pp. 244-250

Haq, I. and Saravanamuttoo, H. I. H., 1993, 'Axial Compressor Fouling Evaluation at High Speed Settings Using an Aerothermodynamic Model,' ASME Paper 93-GT-407

강동진, 1994, '단축적 방법을 이용한 다단 축류압축기의 설계,' 대한기계학회 논문집, 제 18권, 제 6 호, pp. 1598-1603

Cohen, H., Rogers, G. F. C. and Saravanamuttoo, H. I. H., 1996, Gas Turbine Theory, 4th ed., Longman Group Limited, U.K.

강동진, 류제욱, 정평석, 1993, '가스터빈 기관의 탈설계점 해석,' 대한기계학회 논문집, 제 17권, 제 7 호, pp. 1851-1863

Howell, A. R. and Bonham, R. P., 1950, 'Overall and Stage Characteristics of Axial Flow Compressors,' Proc, IMechE, Vol. 163, pp. 235-248

Klapproth, J. F., 1958, discussion in reference (1)

Cyrus, V., 1994, 'Separated Flows in Axial Flow Compressor with Variable Stator Vanes at Positive Incidence Angles', ASME paper 94-GT -480

김동섭, 노승탁, 1996, '단축가스터빈 설계점 및 부분부하 성능해석 프로그램 개발', 대한기계학회논문집 (B), 제 20 권, 제 7 호, pp. 2409-2420

Kashiwabara, Y., Matsuura, Y., Katoh, Y., Hagiwara. N., Hattori, T. and Tokunaga, K., 1986, 'Development of a High-Pressure-Ratio Axial Flow Compressor for a Medium-Size Gas Turbine,' ASME Journal of Turbomachinery, Vol. 108, pp. 233-239

Iwamoto, T., Ikesawa, K., Kanayama, T., Nagai, K., Yukinari, A. and Nakagawa, T., 1991,'Development of a High-Pressure Ratio Axial Flow Compressor,' Proceedings of the 1991 Yokohama International Gas Turbine Congress, Vol. II, pp. 79-86

Herzke, K., 1983, 'Beschreibung des instationaeren Verhaltens von Gasturbinen durch Simulations-modelle,' Dissertation, University of Hannover, Germany