Theoretical Prediction of Limit Cycle Oscillations in Support of Flight Flutter Testing
Abstract
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 31, 2003
- Accession Number
- ADA426408
Entities
People
- Earl H. Dowell
- Kenneth C. Hall
Organizations
- Duke University