Performance characteristics in transonic axial compressor rotor blade using circular jets
The reduction of the flow separation region or even eliminating it from the transonic axial flow compressor has been a motivating research area as it reduces turbulence and modifies the flow field into more desired state. Even a small performance improvement could be a big help in saving fuel cost....
Saved in:
主要作者: | Epsipha, Pauline |
---|---|
格式: | Thesis |
语言: | English |
出版: |
2016
|
主题: | |
在线阅读: | http://psasir.upm.edu.my/id/eprint/70648/1/FK%202016%20151%20-%20IR.pdf |
标签: |
添加标签
没有标签, 成为第一个标记此记录!
|
相似书籍
-
Damage severity evaluation methods for biocomposite vertical axis wind turbine blades due to lightning strikes
由: Mat Daud, Siti Zubaidah
出版: (2018) -
Effect of surface roughness on helicopter main rotor blade
由: Wan Rohizan, Wan Norhafizan
出版: (2017) -
Tribology study on vane coated cylinder of a rotary compressor /
由: Lenny Yusnita Mustapah
出版: (2014) -
Design, development and performance of a disc plough combined with rotary blades
由: Hashemi, Ali
出版: (2012) -
Performance evaluation of aluminide coating on aircraft turbine blade /
由: Siew, Chee Wong
出版: (2012)