Abstract:ENGINEERING NOTES 893 'R 0.99 0.98 0.02 0.01 -----NON MIXING • --MIXING 0 0.02 £ 0.04 0.06 Fig. 2 Effects of fan exit profiles on nozzle thrust and breakeven fan efficiency.
ResultsSample results were calculated for the case where the compressure pressure ratio is 1.5, M 0 = 0.85, and M c = 0.5.The reduction in net thrust of the fanstream vs e is shown in Fig. 2. It can be seen that the mixing losses introduce a substantial penalty. It is also evident that substantial increases in compressor efficiency must be… Show more
scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.