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- W2357572860 abstract "Short Takeoff /Vertical Landing(STOVL)aircraft has been attached importance to by super aviation country on the world due to its superior campaign performance. By referring to the technology development of the most advanced STOVL engine F135-PW-600 at present,research on the matching and constraints of cruise engine and lift fan when developing STOVL engine based on a domestic aeroengine is conducted.The results demonstrate that: with lift fan' s pressure ratio and mass flow rate increasing,cruise engine' s thrust decreases lift fan's thrust increases;at the same cruise engine state,with lift fan's mass flow rate increasing,lift fan' s pressure ratio when engine' s the front and back thrust balance decreases and the total thrust increases;the better the performance of cruise engine is,the higher pressure ratio and mass flow rate of lift fan and total engine thrust are." @default.
- W2357572860 created "2016-06-24" @default.
- W2357572860 creator A5022313890 @default.
- W2357572860 date "2014-01-01" @default.
- W2357572860 modified "2023-09-25" @default.
- W2357572860 title "Performance study of developing STOVL engine based on a certain aeroengine" @default.
- W2357572860 hasPublicationYear "2014" @default.
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