Computational fluid dynamics calculations using high-performance parallel computing were
conducted to simulate the prestall flow of a transonic compressor stage, NASA compressor …

Study of flow instability in turbine engine compressors is crucial to understand the inception
and evolution of engine stall. Aerodynamics experts have been working on detecting the …

Aerodynamic instabilities that naturally occur in compression systems, such as surge and
rotating stall, largely reduce the life duration and performance of system components. The …

A sufficient understanding of the stall behavior is crucial to improve the stability of a
compressor. The stall development process and its sensitive locations in a centrifugal …

A stall inception model of centrifugal compressors is developed on the basis of the global
stability analysis in the present paper. This model takes specific flow patterns and impeller …

High-resolution simulation data sets provide plethora of information, which needs to be
explored by application scientists to gain enhanced understanding about various …

In this paper the concept of 'quasi-dynamic'pressure measurements is introduced and used
in order to obtain compressor spectral maps describing the process of surge onset in a …

THE operating range of axial flow compressors is generally limited by the onset of
aerodynamic instabilities, surge, and rotating stall. Several researchers have reported that …

CoDDA (C opula-based D istribution D riven A nalysis) is a flexible framework for large-
scale multivariate datasets. A common strategy to deal with large-scale scientific simulation …

A numerical study has been carried out to understand the effect of discrete endwall
recirculation on the performance of a transonic axial compressor rotor. Twenty-two …