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Simulation of casing treatments of a transonic compressor stage
M. Hembera,
H. P. Kau
, E. Johann
Chair of Turbomachinery and Flight Propulsion
Technical University of Munich
Rolls-Royce Deutschland
Research output
:
Contribution to journal
›
Article
›
peer-review
53
Scopus citations
Overview
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Keyphrases
Casing Treatment
100%
Transonic Compressor Stage
100%
Stator
50%
Axial Slot
33%
Three-dimensional (3D)
16%
High Pressure
16%
Rotor
16%
Time-accurate
16%
Enhanced Stability
16%
Rotor-stator
16%
Flow Solver
16%
Transonic
16%
Circumferential Direction
16%
Multi-block Grid
16%
Single Rotor
16%
Navier-Stokes Flow
16%
Flow Mechanism
16%
Unsteady Simulation
16%
Stall Margin
16%
Axial Compressor Stage
16%
Axial Extension
16%
Multistage Compressor
16%
Blade Passage
16%
Stator Modes
16%
Engineering
Compressor Stage
100%
Casing Treatment
100%
Rotors
50%
Nodes
16%
Flow Solver
16%
Circumferential Direction
16%
Blade Passage
16%
Flow Mechanism
16%
Axial Compressors
16%
Stage Compressor
16%
Axial Extension
16%
Multistage Compressor
16%