220席級幅広胴体機巡航形態の空力設計
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学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
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- Material Type
- 規格・テクニカルリポート類
- Title
- Author/Editor
- 野村, 聡幸
- Author Heading
- Publication, Distribution, etc.
- Publication Date
- 2026-02-17
- Publication Date (W3CDTF)
- 2026-02-17
- Alternative Title
- Aerodynamic Design of a 220-Seat Class Double-Bubble Passenger Aircraft at Cruise
- Periodical title
- 宇宙航空研究開発機構契約報告
- No. or year of volume/issue
- JAXA-CR-25-002
- Volume
- JAXA-CR-25-002
- ISSN (Periodical Title)
- EISSN : 2433-2240
- Text Language Code
- jpn
- Subject Heading
- Target Audience
- 一般
- Note (General)
- 出版タイプ： VoRThe aerodynamic design of a 220-seat class double-bubble passenger aircraft HELNA0A at cruise is conducted to evaluate the drag-reducing effects of advanced aerodynamic technologies with CFD and wind-tunnel testing. HELNA0A is assumed to have the same technology level as existing aircraft, and its cruise lift-to-drag ratio of 16.58 is obtained through the aerodynamic design.形態: カラー図版ありPhysical characteristics: Original contains color illustrationsレポート番号: JAXA-CR-25-002
- Access Restrictions
- インターネット公開
- 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）
- 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