Abstract
SummaryA study has been made of the effects of inlet coolant injection upon axial compressor performance, using the results of tests on turboshaft engines. It is shown that evaporation of the coolant changes the stage work distribution as well as the ideal compression work and that these effects may be estimated by elementary thermodynamic methods. Simplified prediction procedures are suggested and compared with experimental results.
Publisher
Cambridge University Press (CUP)
Reference4 articles.
1. Mellor G. L. and Root T. Generalised Multi-Stage Axial Compressor Characteristics. ASME Paper 61-Hyd-14. Presented at the ASME-EIC Hydraulic Conference, Montreal,. Canada, 7th-8th May 1961.
2. A Rapid Method for Calculating the “Off-Design” Performance of Compressors and Turbines
3. Drop Size Distribution in Sprays;Nukiyama;Industrial and Engineering Chemistry,1951
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