Investigation of ATP blades(PartI): Test of Thin Airfoils in the NAL 2-D Transonic Wind Tunnel

Material type: 文書・図像類

Author: 佐藤, 衛ほか

Publisher: 航空宇宙技術研究所

Publication date: 1989-11

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: Two-dimensional transonic wind tunnel tests of thin airfoils were made as a part of aerodynamic research on propeller blades for advanced turboprop en...

Search by Bookstore

Holdings of Libraries in Japan

This page shows libraries in Japan other than the National Diet Library that hold the material.

List of Cooperating Institutions and Databases

Please contact your local library for information on how to use materials or whether it is possible to request materials from the holding libraries.

other

JAXA Repository
Digital
You can check the holdings of institutions and databases with which 学術機関リポジトリデータベース（IRDB）（機関リポジトリ） is linked at the site of 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）.
JAXA Repository

Search by Bookstore

Bibliographic Record

You can check the details of this material, its authority (keywords that refer to materials on the same subject, author's name, etc.), etc.

Digital

Material Type: 文書・図像類
Title: Investigation of ATP blades(PartI): Test of Thin Airfoils in the NAL 2-D Transonic Wind Tunnel
Author/Editor: 佐藤, 衛
神田, 宏
須谷, 記和
小国, 保男
馬場, 滋夫
三輪, 等
河本, 巌
少路, 宏和
大竹, 邦彦
菊野, 栄次
市川, 恵通
遠藤, 宏
信谷, 英之
SATO, Mamoru
KANDA, Hiroshi
SUDANI, Norikazu
OGUNI, Yasuo
BABA, Shigeo
MIWA, Hitoshi
KAWAMOTO, Iwao
SHOJI, Hirokazu
OOTAKE, Kunihiko
KIKUNO, Eiji
ICHIKAWA, Yoshimichi
ENDO, Hiroshi
NOBUTANI, Hideyuki
Author Heading: 佐藤, 衛
神田, 宏
須谷, 記和
小国, 保男
馬場, 滋夫
三輪, 等
河本, 巌
少路, 宏和
大竹, 邦彦
菊野, 栄次
市川, 恵通
遠藤, 宏
信谷, 英之
SATO, Mamoru
KANDA, Hiroshi
SUDANI, Norikazu
OGUNI, Yasuo
BABA, Shigeo
MIWA, Hitoshi
KAWAMOTO, Iwao
SHOJI, Hirokazu
OOTAKE, Kunihiko
KIKUNO, Eiji
ICHIKAWA, Yoshimichi
ENDO, Hiroshi
NOBUTANI, Hideyuki
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1989-11
Publication Date (W3CDTF): 1989-11
Alternative Title: ATPブレードの研究(I): 薄翼の遷音速二次元風洞試験
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: 615
Volume: 615
Pages: 48-
ISSN (Periodical Title): ISSN : 0452-2982
Text Language Code: eng
Target Audience: 一般
Note (General): Two-dimensional transonic wind tunnel tests of thin airfoils were made as a part of aerodynamic research on propeller blades for advanced turboprop engines. The test airfoils were NACA-16-202 and NACA16-204 which were developed as airfoils for conventional propeller systems at NACA in 1934. The Reynolds number is 8×106. The Mach number was varied from 0.6 to 1.0 and angles of attack from -10 to +16. In addition, vibration characteristics were measured and analyzed.
資料番号: NALTM0615000
レポート番号: NAL TM-615
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44198&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44198&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