Aeroelastic Analysis of a Distributed Electric Propulsion Wing
| Autor: | Carol D. Wieseman, Bret Stanford, Steven J. Massey, Jennifer Heeg |
|---|---|
| Rok vydání: | 2017 |
| Předmět: |
020301 aerospace & aeronautics
Engineering Wing business.industry 02 engineering and technology Aerodynamics Structural engineering Computational fluid dynamics Aeroelasticity 01 natural sciences Finite element method 010305 fluids & plasmas Physics::Fluid Dynamics 0203 mechanical engineering Electrically powered spacecraft propulsion 0103 physical sciences Flutter Dynamic pressure business |
| Zdroj: | 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. |
| DOI: | 10.2514/6.2017-0413 |
| Popis: | An aeroelastic analysis of a prototype distributed electric propulsion wing is presented. Results using MSC Nastran (Registered Trademark) doublet lattice aerodynamics are compared to those based on FUN3D Reynolds Averaged Navier- Stokes aerodynamics. Four levels of grid refinement were examined for the FUN3D solutions and solutions were seen to be well converged. It was found that no oscillatory instability existed, only that of divergence, which occurred in the first bending mode at a dynamic pressure of over three times the flutter clearance condition. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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