JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

このアイテムに関連するファイルはありません。

タイトルUpstream Swirl Effects on the Flow Inside a Labyrinth Seal
著者(英)Johnson, Mark C.; Morrison, Gerald L.
著者所属(英)Texas A&M Univ.
発行日1997-05-01
言語eng
内容記述The flow field inside a seven cavity tooth on rotor labyrinth seal was measured using a 3D laser Doppler anemometer system. The seal was operated at a Reynolds number of 24,000 and a Taylor number of 6,600 using water as the working fluid. Swirl vanes were placed upstream of the seal to produce positive, negative, and no preswirl. It was found that the axial and radial velocities were minimally effected. The tangential velocity, both in the clearance region and the seal cavities on the rotor, were greatly altered by the preswirl. By applying negative preswirl, the tangential velocity was suppressed, even in the seventh cavity. The turbulence levels decreased as the preswirl varied from negative to positive.
NASA分類Mechanical Engineering
レポートNO97N24535
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/541533


このリポジトリに保管されているアイテムは、他に指定されている場合を除き、著作権により保護されています。