Print Email Facebook Twitter Aeroelastic analysis of quasi-axisymmetrical airships at low Mach number Part of: ECCOMAS CFD 2006: Proceedings of the European Conference on Computational Fluid Dynamics· list the conference papers Title Aeroelastic analysis of quasi-axisymmetrical airships at low Mach number Author Destuynder, P. Santi, F. Date 2006-09-05 Abstract An aeroelastic modelling of an axisymmetrical airship is discussed in this paper. The main difficulty is due to the fact that instabilities are not axisymmetrical. Furthermore an Euler-Lagrange kinematical coupling is necessary in order to represent the fluid-structure interaction. Our strategy is based on some arbitrary change of domain (for the air flow) which are governed by the movement of the structure. Some numerical results illustrate the method. Subject fluid dynamicsaeroelasticitystabilityairship technology To reference this document use: http://resolver.tudelft.nl/uuid:c62cd184-4ca3-49e0-adc1-a124639471f6 Part of collection Conference proceedings Document type conference paper Rights (c) 2006 Destuynder, P.; Santi, F. Files PDF Destuynder.pdf 637.49 KB Close viewer /islandora/object/uuid:c62cd184-4ca3-49e0-adc1-a124639471f6/datastream/OBJ/view