Theoretical Prediction of Limit Cycle Oscillations in Support of Flight Flutter Testing
Final technical rept. 2002-2003
DUKE UNIV DURHAM NC DEPT OF MECHANICALENGINEERING AND MATERIALS SCIENCE
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Using a novel harmonic balance method and a state of the art computational fluid dynamics CFD model, limit cycle oscillations have been calculated for a conventional and supercritical airfoil as well as the F-16 wing. The latter result is the first of its kind.
- Attack and Fighter Aircraft
- Fluid Mechanics