Effect of Bypass Ratio on Optimal Fan Outer Pressure Ratio and Performance for Turbofan Engines
Authors:
- 2 January 2019
- journal article
- research article
- Published by Springer Nature in International Journal of Aeronautical and Space Sciences
- Vol. 20 (1) , 157-164
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China (51706170)
- Postdoctoral Research Foundation of China (2017M623185)
This publication has 2 references indexed in Scilit:
- Optimum Fan Pressure Ratio for Bypass Engines with Separate or Mixed Exhaust StreamsJournal of Propulsion and Power, 2001
- Identifying Optimal Fan Compressor Pressure Ratios for the Mixed-Stream Turbofan EngineJournal of Propulsion and Power, 2000