Aeroelastic wind tunnel model for tail buffeting analysis using rapid prototyping technologies
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DOI: 10.1007/s13272-021-00523-9
Abstract: Modern high-agility aircraft are often subjected to tail buffeting at moderate subsonic Mach numbers and medium to high angles of attack. The excitation of the tail structures through the unsteady flow field can lead to… read more here.
Keywords: tail buffeting; model; tunnel; wind tunnel ... See more keywords