National Aerospace Laboratory
National Aerospace Laboratory
National Aerospace Laboratory
Ishikawajima-Harima Heavy Industries Co Ltd
Ishikawajima-Harima Heavy Industries Co Ltd
Ishikawajima-Harima Heavy Industries Co Ltd
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory (NAL)
雑誌名
航空宇宙技術研究所特別資料
雑誌名(英)
Special Publication of National Aerospace Laboratory
巻
30
ページ
87 - 91
発行年
1996-01
会議概要（会議名, 開催地, 会期, 主催者等）
航空宇宙技術研究所 7-9 Jun. 1995 東京 日本
会議概要（会議名, 開催地, 会期, 主催者等）（英）
National Aerospace Laboratory 7-9 Jun. 1995 Tokyo Japan
The viscous flow through a fan with an inlet distortion was calculated. The inlet distortion was given as a total pressure defect in the 1/3 area of circumferential direction. The distortion is actually stationary, however, the phenomenon becomes unsteady since the distorted flow beats the rotor blade row periodically. Therefore an unsteady Navier-Stokes code was utilized. Computational result was extremely enormous and the validity of the computation has been qualitatively confirmed by means of the visualization technique using animation video images.
インレットディストーションのあるファン翼列の非定常流れ解析
nalsp0030016.pdf
(486.14KB)
