Uncertainty effects of blade geometric deviations on the aerodynamic stability of a high-load transonic axial compressor
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy
Published online on June 05, 2026
Abstract
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, Ahead of Print.
This study examines the impact of manufacturing deviations in blade geometry (stagger angle, thickness, chord length, leading edge radius, and trailing edge radius) on the stability margin (SM) of a high-load transonic axial-flow compressor. Following the ...
This study examines the impact of manufacturing deviations in blade geometry (stagger angle, thickness, chord length, leading edge radius, and trailing edge radius) on the stability margin (SM) of a high-load transonic axial-flow compressor. Following the ...