逆解法を用いた翼胴一体化設計について

Material type: 文書・図像類

Author: 谷, 泰寛ほか

Publisher: 航空宇宙技術研究所

Publication date: 1990-11

Material Format: Digital

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Note (General)：: In this paper, an iterative design procedure is described for three dimensional wing-body configuration, especially blended wing-body configuration, u...

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Material Type: 文書・図像類
Title: 逆解法を用いた翼胴一体化設計について
Author/Editor: 谷, 泰寛
越岡, 康弘
廣瀬, 秀大
Tani, Yosuhiro
Koshioka, Yasuhiro
Hirose, Hidehiro
Author Heading: 谷, 泰寛
越岡, 康弘
廣瀬, 秀大
Tani, Yosuhiro
Koshioka, Yasuhiro
Hirose, Hidehiro
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1990-11
Publication Date (W3CDTF): 1990-11
Alternative Title: Blended Wing-Body Configuration Design using Transonic Inverse Code
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-14
No. or year of volume/issue: 14
Volume: 14
Pages: 115-120
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): In this paper, an iterative design procedure is described for three dimensional wing-body configuration, especially blended wing-body configuration, using a three dimensional transonic inverse method with target pressure distribution. In this application, it is combined with a full potential analysis code. Some of the design results for a conventional and a blended wing-body configuration are presented. Also a finite volume Euler solver is applied to analyze the designed configurations.
資料番号: NALSP0014018
レポート番号: NAL SP-14
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43451&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43451&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