A Gas Turbine Compressor Simulation Model for Inclusion of Active Control Strategies

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.

Publication Info

Category

Type

Conference

Author

C. Cravero, A.F. Massardo

Journal

RTO Symposium on Active Control Technology for Enchanced Performances Operational Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles, Braunschweig, 8-11- May 2000

Year

2000

DOI / Link to the paper

Paper ID

2000-TPG-4