ファンジェットSTOL実験機模型の地面効果試験

Material type: 文書・図像類

Author: STOLプロジェクト推進本部実験機開発室空力技術開発チームほか

Publisher: 航空宇宙技術研究所

Publication date: 1984-08

Material Format: Digital

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Note (General)：: To investigate the basic aerodynamic characteristics of the turbofan powered-lift STOL aircraft near the ground, wind tunnel tests were made on the 8％...

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Material Type: 文書・図像類
Title: ファンジェットSTOL実験機模型の地面効果試験
Author/Editor: STOLプロジェクト推進本部実験機開発室空力技術開発チーム
Aerodynamics Team Research Aircraft Development Section STOL Aircraft Project Group
Author Heading: STOLプロジェクト推進本部実験機開発室空力技術開発チーム
Aerodynamics Team Research Aircraft Development Section STOL Aircraft Project Group
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1984-08
Publication Date (W3CDTF): 1984-08
Alternative Title: Low-Speed Wind Tunnel Tests of the NAL Fan-Jet STOL-Research-Aircraft Model with Ground Simulation by Tangential Blowing
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-828
No. or year of volume/issue: 828
Volume: 828
Pages: 105-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): To investigate the basic aerodynamic characteristics of the turbofan powered-lift STOL aircraft near the ground, wind tunnel tests were made on the 8％ NAL Quiet STOL Research Aircraft complete model with an upper surface blowing flap system in the NAL 6.5m×5.5m low speed wind tunnel. The wind tunnel tests were conducted using a fixed ground plane with tangential blowing boundary-layer control instead of a moving belt ground plane. The tests covered the effects on longitudinal and lateral static stability produced by variations of flap angle and engine thrust, and by ground proximity. Some of the more significant effects of ground proximity include appreciable changes in six-component force and moment once jet impingment occured. These data obtained in the wind tunnel tests were offered for analysis of flying qualities of the NAL Quiet STOL Research Aircraft.
資料番号: NALTR0828000
レポート番号: NAL TR-828
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45086&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45086&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