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This document summarizes a study on inviscid flow calculation around a flexible airship. It uses an unsteady Euler model for the fluid part coupled with elastodynamic equations for the flexible structure. The numerical model is based on a mixed element volume discretization in an arbitrary Lagrangian-Eulerian framework to handle structural deformations. Several inviscid flow calculations are performed around a prolate spheroid airship model to evaluate aerodynamic coefficients and study the effects of struc

Author

Manu Chakkingal

Language

EN