A Gas Turbine Compressor Simulation Model for Inclusion of Active Control Strategies
GENOVA UNIV (ITALY)
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A one dimensional time-marching model to solve the dynamic behavior of a compression system is presented. The computational method is described in some details and it is applied to a three-stage axial compressor with different plenum configurations. This computational model for the simulation of a multistage axial compressor is used to investigate the insertion of an active control system.
- Computer Programming and Software
- Hydraulic and Pneumatic Equipment
- Jet and Gas Turbine Engines