Author:
Doyle M. D. C.,Dixon S. L.
Abstract
SummaryA method of calculation is developed to compute the overall performance of a multi-stage axial compressor, from a knowledge of the individual stage characteristics, by a “stacking” technique. Compressor models are designed and their overall performance calculated. These results are compared to show, qualitatively, the effect of alterations in design and stage performance on overall performance and to find how compressors should be designed for optimum performance.
Publisher
Cambridge University Press (CUP)
Reference6 articles.
1. Effects of Stage Characteristics and Matching on Axial Flow Compressor Performance;Stone;Transactions of the American Society of Mechanical Engineers,1958
2. Benser W. A. Aerodynamic Design of Axial Flow Compressors. Chapter XIII. N.A.C.A. RM 56 B03b, 1956.
3. Some Stall and Surge Phenomena in Axial Flow Compressors;Huppert;Journal of the Aeronautical Sciences,1953
4. Iura T. and Rannie W. D. Observations of Propagating Stall in Axial Flow Compressors. Report No. 4. Mechanical Engineering Laboratory, California Institute of Technology, April 1953. (Navy Contract N6-ORI-102 Task Order 4.)
Cited by
11 articles.
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