Ishikawajima-Harima Heavy Industries Co. Ltd.
Ishikawajima-Harima Heavy Industries Co. Ltd.
National Aerospace Laboratory
National Aerospace Laboratory
National Aerospace Laboratory
National Aerospace Laboratory
National Aerospace Laboratory
出版者
宇宙航空研究開発機構
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構特別資料
雑誌名(英)
JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop)
巻
JAXA-SP-06-029E
ページ
180 - 183
発行年
2007-03-30
会議概要（会議名, 開催地, 会期, 主催者等）
SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design 航空宇宙技術研究所 19980316-19980317 東京 日本
会議概要（会議名, 開催地, 会期, 主催者等）（英）
SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design National Aerospace Laboratory 19980316-19980317 Tokyo Japan
抄録（英）
A three-dimensional time-accurate Reynolds-averaged Navier-Stokes code has been extended for use in a parallel supercomputer called Numerical Wind Tunnel (NWT) developed by the Japanese National Aerospace Laboratory. The power of parallel supercomputer enables us to perform a more accurate computation of the unsteady flowfield within a multipassage configuration. The numerical simulations was aimed at investigating the unsteady flow behavior for a transonic fan rotor blade with inlet total pressure distortion, which is inclined to appear in a SST (SuperSonic Transport) propulsion system.
Unsteady flow analysis of fan rotor with inlet distortion
63609020.pdf
(1.36MB)
