AN INVESTIGATION OF STABILITY IN THE LAR
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A.P. LEWIS
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Article
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2002
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Elsevier Science
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English
โ 475 KB
It is well known that the presence of non-linearities may signi"cantly a!ect the aeroelastic response of an aerospace vehicle structure. In this paper, the aeroelastic behaviour at high Mach numbers of an all-moving control surface with a non-linearity in the root support is investigated. Very often