Effects of stator splitter blades on aerodynamic performance of a single-stage transonic axial compressor

Splitter blades located between stator blades in a single-stage axial compressor were proposed and investigated in this work to find their effects on aerodynamic performance and operating stability. Aerodynamic performance of the compressor was evaluated using three-dimensional Reynolds-averaged Na...

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Auteurs principaux:	Ky-Quang Pham, Xuan-Truong Le, Cong-Truong Dinh
Format:	Artigo
Langue:	Inglês
Publié:	Universiti Malaysia Pahang Al-Sultang Abdullah Publishing 2020-12-01
Collection:	Journal of Mechanical Engineering and Sciences
Sujets:	Transonic axial compressor stator splitter blades RANS analysis total pressure ratio adiabatic efficiency stall margin
Accès en ligne:	http://journal.ump.edu.my/jmes/article/view/3358
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