遷音速後退翼に対する境界層効果の評価

Material type: 文書・図像類

Author: 小松, 浩司ほか

Publisher: 航空宇宙技術研究所

Publication date: 1984-11

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: A comparison of the result of numerical analysis with experimental data is made for the ONERA M-6 and the practical transonic wing model 720211. The J...

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: 遷音速後退翼に対する境界層効果の評価
Author/Editor: 小松, 浩司
飯田, 栄治
河村, 龍馬
廣瀬, 直喜
松野, 謙一
Komatsu, Koji
Iida, Eiji
Kawamura, Ryuma
Hirose, Naoki
Matsuno, Ken-ichi
Author Heading: 小松, 浩司
飯田, 栄治
河村, 龍馬
廣瀬, 直喜
松野, 謙一
Komatsu, Koji
Iida, Eiji
Kawamura, Ryuma
Hirose, Naoki
Matsuno, Ken-ichi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1984-11
Publication Date (W3CDTF): 1984-11
Alternative Title: The Analysis of Practical Transonic Swept Wings with and without Boundary Layer Effects
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-3
No. or year of volume/issue: 3
Volume: 3
Pages: 305-312
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): A comparison of the result of numerical analysis with experimental data is made for the ONERA M-6 and the practical transonic wing model 720211. The Jameson-Caughey's transonic wing programs FLO22 and FLO27 are used. The wing aerodynamic characteristics with viscous effect are evaluated by taking into account the boundary layer friction drag. This drag is calculated by using a three-dimensional compressible boundary layer program for wings, BLAY. Finally, a viscous-inviscid interaction procedure for FLO27-BLAY is proposed, and a preliminary result is presented.
資料番号: NALSP0003035
レポート番号: NAL SP-3
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43177&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43177&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