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Investigation of an anomalous flow condition of the Langley pilot model expansion tube
本文(外部サイト)http://hdl.handle.net/2060/19740023645
著者(英)Friesen, W. J.
著者所属(英)NASA Langley Research Center
発行日1974-08-01
言語eng
内容記述Free-stream flow velocity measurements were made in the Langley pilot model expansion tube during the test flow interval. During this interval, an anomalous dip in pitot pressure occurs for the expansion tube operating conditions employed. Within the test flow interval, the main conclusions reached from comparison of the measured flow velocity, pitot pressure, and tube wall pressure are: the variations which occur in velocity and wall pressure are small compared with the variations in pitot pressure; a corresponding dip in the derived flow density is associated with the dip in pitot pressure; and the value of the average density over the interval, which results from the expansion from the shocked intermediate chamber condition, is approximately one-half of the value that can result from only an isentropic process.
NASA分類FLUID MECHANICS
レポートNO74N31758
NASA-TN-D-7704
L-9633
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/193282


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。