航空機開発における風洞試験とCFD

Material type: 文書・図像類

Author: 高梨, 進ほか

Publisher: 航空宇宙技術研究所

Publication date: 1991-12

Material Format: Digital

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Note (General)：: In this paper, the roles of wind tunnel testing and computational fluid dynamics (CFD) in the aircraft development is briefly described. The stress is...

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Material Type: 文書・図像類
Title: 航空機開発における風洞試験とCFD
Author/Editor: 高梨, 進
Takanashi, Susumu
Author Heading: 高梨, 進
Takanashi, Susumu
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1991-12
Publication Date (W3CDTF): 1991-12
Alternative Title: On the Roles of Wind Tunnel Testing and Computational Fluid Dynamics in the Aircraft Development
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-16
No. or year of volume/issue: 16
Volume: 16
Pages: 313-318
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): In this paper, the roles of wind tunnel testing and computational fluid dynamics (CFD) in the aircraft development is briefly described. The stress is put on the importance of CFD as an aerodynamic design tool to drastically reduce both cost and period of development. Prior to the application of CFD to practical design problem, the existing CFD codes must be verified with the reliable experimental data. A demonstrative example of CFD validation is presented to show the state of the arts of CFD by comparing the Navier-Stokes simulation results with the transonic wind tunnel test data for a NACA0012 airfoil at several angles of attack. The importance of application of CFD to inverse design problem is also discussed.
資料番号: NALSP0016049
レポート番号: NAL SP-16
Access Restrictions: 限定公開
Periodical Title (NCID): AN10097345
https://ci.nii.ac.jp/ncid/AN10097345
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ