ムービングベルト式地面効果試験装置

Material type: 文書・図像類

Author: 野中, 修ほか

Publisher: 航空宇宙技術研究所

Publication date: 1998-02

Material Format: Digital

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Note (General)：: 航空機模型の離着陸時の地面効果を評価するために、ムービングベルト式の地面効果試験装置が1995年3月に大型低速風洞に完成した。ここでは、本装置の構成と特性について述べる。A moving belt type ground effect measurement system was construct...

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Material Type: 文書・図像類
Title: ムービングベルト式地面効果試験装置
Author/Editor: 野中, 修
萱場, 重男
林, 良生
Nonaka, Osamu
Kayaba, Shigeo
Hayashi, Yoshio
Author Heading: 野中, 修
萱場, 重男
林, 良生
Nonaka, Osamu
Kayaba, Shigeo
Hayashi, Yoshio
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1998-02
Publication Date (W3CDTF): 1998-02
Alternative Title: Moving belt ground effect testing system of NAL 6.5 x 5.5 m low speed wind tunnel
Periodical title: 航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
No. or year of volume/issue: 724
Volume: 724
Pages: 1-30
ISSN (Periodical Title): ISSN : 0452-2982
Text Language Code: jpn
Subject Heading: 地面効果試験装置
低速風洞
ムービングベルト装置
ベルト走行特性
気流特性
境界層吸込
静圧分布
乱れ分布
地面板
ground effect testing system
low speed wind tunnel
moving belt system
belt running characteristic
flow characteristic
boundary layer suction
static pressure distribution
turbulent distribution
ground plane
Target Audience: 一般
Note (General): 航空機模型の離着陸時の地面効果を評価するために、ムービングベルト式の地面効果試験装置が1995年3月に大型低速風洞に完成した。ここでは、本装置の構成と特性について述べる。
A moving belt type ground effect measurement system was constructed to evaluate ground effect characteristics of aircraft models at the NAL low speed wind tunnel facility in March 1995. This paper summarizes the hardware and function of this equipment. Some function tests and flow characteristic tests were carried out, with this equipment installed in the test section. Some effects of the following parameters to drive this system on the flow above the belt plane are indicated: (1) belt running speed; (2) boundary layer suction; and (3) rear flap of ground plane. These parameters were adjusted to the optimum values experimentally. Some experimental results on the following items are indicated: (1) static pressure distribution along the wind tunnel axis on the moving plane; (2) turbulent distribution on the moving plane; and (3) boundary layer velocity profile on the moving plane.
資料番号: AA0001439000
レポート番号: NAL TM-724
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=40182&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=40182&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