Numerical simulation with bleed and bypass effects of nacelles on SST

Autor:	Kaiden, Takeshi, Shibata, Makoto, Iwamiya, Toshiyuki
Jazyk:	angličtina
Rok vydání:	2007
Předmět:	境界層剥離 airframe shock wave 衝撃波 超音速機 lift drag ratio boundary layer separation 民間航空 揚抗比 計算流体力学 computational fluid dynamics separated flow バイパス効果 civil aviation 機体 nacelle 剥離流 ナセル bypass effect 航空機設計 supersonic aircraft aircraft design
Zdroj:	宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop). :10-19
ISSN:	1349-113X
Popis:	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 SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design National Aerospace Laboratory 19980316-19980317 Tokyo Japan 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. 資料番号: AA0063609002 レポート番号: JAXA-SP-06-029E
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=jairo_______::662874516feff075d7bc2cf407e8d21e http://id.nii.ac.jp/1696/00005727/ Zobrazit plný text záznamu