渦格子法による同軸反転型高速プロペラの解析

Material type: 文書・図像類

Author: 齊藤, 茂ほか

Publisher: 航空宇宙技術研究所

Publication date: 1990-11

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: Aerodynamic performance of a counter-rotating propeller has been calculated by means of Vortex Lattice Method. The new wake system of the each rotor w...

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: 渦格子法による同軸反転型高速プロペラの解析
Author/Editor: 齊藤, 茂
溝渕, 泰寛
Saito, Shigeru
Mizobuchi, Yasuhiro
Author Heading: 齊藤, 茂
溝渕, 泰寛
Saito, Shigeru
Mizobuchi, Yasuhiro
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1990-11
Publication Date (W3CDTF): 1990-11
Alternative Title: Analysis of the Aerodynamic Performance of Counter-Rotating Propeller by Means of Vortex Lattice Method
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: 227-232
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): Aerodynamic performance of a counter-rotating propeller has been calculated by means of Vortex Lattice Method. The new wake system of the each rotor was constructed using a prescribed wake model by Kocurek-Berkowitz-Harris, which is well known as an empirical wake system of helicopter rotor with low aspect ratio blade. The votex filaments including a blade tip vortex were treated as vortex tube with the finite vortex core in order to avoid the numerical divergence in the calculation. The calculated results for a single-rotating propeller have shown a good agreement with experimental results in the subsonic speed range. The results for a counter-rotating propeller have compared with those by Local Circulation Method and wind tunnel test results and shown a good correlation.
資料番号: NALSP0014036
レポート番号: NAL SP-14
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43469&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43469&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