Preliminary Assessment of Geometric Variability Effects Through a Viscous Through-Flow Model Applied to Modern Axial-Flow Compressor Blades
An important question for turbomachine designers is how to deal with blade and flowpath geometric variabilities stemming from the manufacturing process or erosion during the component lifetime. The challenge consists of identifying where stringent manufacturing tolerances are absolutely necessary an...
Saved in:
Main Authors: | Arnaud Budo, Jules Bartholet, Thibault Le Men, Koen Hillewaert, Vincent E. Terrapon |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2025-04-01
|
Series: | International Journal of Turbomachinery, Propulsion and Power |
Subjects: | |
Online Access: | https://www.mdpi.com/2504-186X/10/2/6 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
An introduction to viscous flow /
by: Hughes, William F.
Published: (1979) -
Viscous fluid flow /
by: White, Frank Mangrem
Published: (1974) -
Performance simulation of multi-stage axial-flow compressor of turbo-shaft engine with account for erosive wear nonlinearity of its blades
by: V. A. Potapov, et al.
Published: (2020-10-01) -
STATISTICAL ANALYSIS OF DAMAGEABILITY OF THE BYPASS ENGINES COMPRESSOR BLADES
by: B. A. Chichkov, et al.
Published: (2018-03-01) -
Direct Numerical Simulation of Flow and Heat Transfer in a Compressor Blade Passage Across a Range of Reynolds Numbers
by: Yang Liu, et al.
Published: (2025-06-01)