Abstract
Flight stability is an interesting subject for the researchers and engineers working on design and development of flying objects. This subject will be more complicated when the body free oscillation and its mutual influence are added to it. In present investigation, a three-dimensional free oscillating body (unstable inherently) with a flexible strip attached to its trailing edge which utilized for stabilizing, is studied in a viscous subsonic flow. Navier–Stokes equations are used for fluid flow analysis and Euler–Bernoulli cantilevered beam is implemented for structure deflection modeling. For analyzing Fluid-Structure Interaction, an iterative partitioned coupling algorithm is utilized. With combining a dynamic simulation tool for body dynamics, the Body-Fluid-Structure Interaction (BFSI) is studied and analyzed. Consequently, an efficient framework is developed for multi-disciplinary analysis of highly flexible stabilizers.
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Kiani, A., Mohammadi-Amin, M. (2020). Body-Fluid-Structure Interaction Simulation for a Trailing-Edge Flexible Stabilizer. In: Kecskeméthy, A., Geu Flores, F. (eds) Multibody Dynamics 2019. ECCOMAS 2019. Computational Methods in Applied Sciences, vol 53. Springer, Cham. https://doi.org/10.1007/978-3-030-23132-3_29
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DOI: https://doi.org/10.1007/978-3-030-23132-3_29
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