Investigation of Stall Flutter in Thermal Turbomachinery (FWF J01022-AST)

Project: Research project

Project Details


The objective of this project was the development of a numerical code for calculation of unsteady, viscous and compressible 2D flow through oscillating casacdes. Special care was put on the prediction of separated flow phenomena.
Effective start/end date1/01/9431/01/95


Explore the research topics touched on by this project. These labels are generated based on the underlying awards/grants. Together they form a unique fingerprint.