The phrase "axial flow compressor" is correct and usable in written English.
It can be used in contexts related to engineering, aerodynamics, or mechanical systems, specifically when discussing types of compressors used in various applications.
Example: "The axial flow compressor is essential for increasing the efficiency of jet engines."
Alternatives: "axial compressor" or "flow compressor".
The compressor of the front stages is transonic three-stage axial flow compressor.
The excitation of acoustic modes in the annulus of a single stage, low speed, axial flow compressor was investigated experimentally.
1D meanline analysis is used for performance prediction of a multi-stage axial flow compressor with VGVs.
A study is made of the conditions in which vibration of the blades of an axial flow compressor can be excited by acoustic resonances of the annulus.
Parametric study of tip injection was implemented experimentally on a subsonic axial flow compressor to understand the underlying flow mechanisms of stability improvement of the compressor with discrete tip injection.
Partial surge is a new type of instability inception observed in a transonic axial flow compressor; it occurs in the form of axisymmetric low-frequency disturbances localized in the hub region and finally grows into rotating stall.
Axial flow compressors are also used to pump gases.
The axial flow compressors are found to be better in meeting the needs of larger engines.
With axial flow compressors as background, the present paper carried out studies on 'interaction of unsteady separated flow over multi-bodies moving relatively in the same flow field'.
The design and performance prediction of axial flow compressors and turbines has been based upon the measurements of the flow-through two-dimensional cascades of blades.
Transonic axial flow compressors are fundamental components in aircraft engines as they make it possible to maximize pressure ratios per stage unit.
