年次大会講演論文集
Online ISSN : 2433-1325
セッションID: 1710
会議情報
無尾翼機の運動解析と重心移動による姿勢制御(G05-2 物体に働く流体力,G05 流体工学部門一般講演)
竪山 弘哲大上 芳文
著者情報
会議録・要旨集 フリー

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抄録
A tailless aircraft suffers from low stability because its momentum arm is short. Therefore, the margin of the position of the center of gravity is limited. As a way of improving the stability, Plank wing, washout and swept wing are usually adopted, which is not suitable for the tailless aircraft of light body and low drag coefficient. In this paper, simulations are conducted to realize high stability of this aircraft by moving the center of gravity, and found out that the longitudinal stability is improved by this technique.
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© 2004 一般社団法人日本機械学会
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