Mitsubishi Heavy Industries Ltd.
Japan Aircraft Development Corporation
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
10 - 19
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）
Supersonic transport is aero-designed with the consideration of the integration between airframe and engine nacelles to utilize the shock wave from them. At the high speed flight, the bleed and bypass air is blown outside from nacelle surface to prevent the flow separation at the compression surface and to control the mass flow to the engine. Therefore it is necessary to assess the aerodynamic interference by blowing. It is here reported that the aero-interference phenomena by blowing from nacelles are obtained by Navier-Stokes solver with overset grids.
Numerical simulation with bleed and bypass effects of nacelles on SST
63609002.pdf
(2.93MB)
