A one-dimensional stage un-stacking approach to reveal flow angles and speeds in a multistage axial compressor at the design operating point
Stage stacking methods commonly use a one-dimensional (1D) through flow analysis at the mean line to design individual axial compressor stages and stack these to form a multistage axial compressor. This phase of design exerts a great influence on each stage's pressure and temperature ratio. The...
Main Authors: | Koh, Alan Fu Hai, Ng, Eddie Yin Kwee |
---|---|
Other Authors: | Energy Research Institute @ NTU (ERI@N) |
Format: | Journal Article |
Language: | English |
Published: |
2019
|
Subjects: | |
Online Access: | https://hdl.handle.net/10356/90003 http://hdl.handle.net/10220/49888 |
Similar Items
-
Stator re-stagger optimization in multistage axial compressor
by: Jinguang Yang, et al.
Published: (2021-06-01) -
Interstage Pressures of a Multistage Compressor with Intercooling
by: Helen Lugo-Méndez, et al.
Published: (2021-03-01) -
Isobaric Expansion Engines–Compressors: Thermodynamic Analysis of Multistage Vapor Driven Compressors
by: Alexander Kronberg, et al.
Published: (2023-09-01) -
The Application of a Laser-Printed Miniature Five-Hole Probe in the End-Wall Flow Measurement of a Multistage Axial Compressor
by: Shuai Ma, et al.
Published: (2023-12-01) -
Axial-flow compressors : a strategy for aerodynamic design and analysis /
by: 250666 Aungier, Ronald H.
Published: (2003)