B747の空力数値シミュレーションと風試によるその精度の検証

Material type: 文書・図像類

Author: 伊藤, 良三ほか

Publisher: 航空宇宙技術研究所

Publication date: 1989-11

Material Format: Digital

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Note (General)：: The viscous transonic flow simulations over B747 wing-fuselage combination were carried out using the three-dimensional Reynolds-averaged thin-layer N...

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Material Type: 文書・図像類
Title: B747の空力数値シミュレーションと風試によるその精度の検証
Author/Editor: 伊藤, 良三
佐藤, 求
高梨, 進
藤井, 孝蔵
松島, 紀佐
Ito, Ryozo
Sato, Motomu
Takanashi, Susumu
Fujii, Kozo
Matsushima, Kisa
Author Heading: 伊藤, 良三
佐藤, 求
高梨, 進
藤井, 孝蔵
松島, 紀佐
Ito, Ryozo
Sato, Motomu
Takanashi, Susumu
Fujii, Kozo
Matsushima, Kisa
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1989-11
Publication Date (W3CDTF): 1989-11
Alternative Title: Numerical Simulation of Transonic Flows Over Boeing-747 and its Validation by Comparison with Experimental Data
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-10
No. or year of volume/issue: 10
Volume: 10
Pages: 237-242
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): The viscous transonic flow simulations over B747 wing-fuselage combination were carried out using the three-dimensional Reynolds-averaged thin-layer Navier-Stokes equations. The single grid system in C-O topology is used for these computations, and it has 1.1 million grid-points. Computed results such as total lift and pressure distributions on the wing are in good agreement with the wind tunnel test data.
資料番号: NALSP0010040
レポート番号: NAL SP-10
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43369&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43369&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
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