This paper summarizes the plans for the second AIAA Aeroelastic Prediction Workshop. The workshop is designed to assess the state-of-the-art of computational methods for predicting unsteady flow fields and aeroelastic response. The goals are to provide an impartial forum to evaluate the effectiveness of existing computer codes and modeling techniques, and to identify computational and experimental areas needing additional research and development. This paper provides guidelines and instructions for participants including the computational aerodynamic model, the structural dynamic properties, the experimental comparison data and the expected output data from simulations. The Benchmark Supercritical Wing (BSCW) has been chosen as the configuration for this workshop. The analyses to be performed will include aeroelastic flutter solutions of the wing mounted on a pitch-and-plunge apparatus.
Plans and Example Results for the 2nd AIAA Aeroelastic Prediction Workshop
2015
19 pages
Report
Keine Angabe
Englisch
Algebra, Analysis, Geometry, & Mathematical Logic , Fluid Mechanics , Aircraft , Test Facilities & Equipment , Aeroelasticity , Predictions , Dynamic structural analysis , Unsteady flow , Wind tunnel tests , Computational fluid dynamics , Supercritical wings , Forced vibration , Steady state , Aerodynamic coefficients , Flutter analysis , Lessons learned , Wind tunnel models , Transonic wind tunnels , Computerized simulation , Finite element method , Nastran , Computational grids
Plans and Example Results for the 2^n^d AIAA Aeroelastic Prediction Workshop (AIAA 2015-0437)
British Library Conference Proceedings | 2015
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