During testing, an experimental forward-swept fan encountered flutter at part-speed conditions. A three-dimensional propulsion aeroelasticity code, based on a computational fluid dynamics (CFD) approach, was used to model the aeroelastic behavior of this fan. This paper describes the flutter calculations and compares the results to the experimental measurements. Results of sensitivity studies are also presented that show the relative importance of different aspects of aeroelastic modeling.
Flutter Calculations for an Experimental Fan
CEAS/AIAA/NVvL International Forum of Aeroelasticity and Structural Dynamics ; 2003 ; Amsterdam, Netherlands
01.01.2003
Preprint
Keine Angabe
Englisch
The technique of flutter calculations
TIBKAT | 1954
|An approximation simplifying wing flutter calculations
TIBKAT | 1951
|Repetitive Flutter Calculations in Structural Design
AIAA | 1976
|