IHI航空エンジンにおける風洞実験とCFD

Material type: 文書・図像類

Author: 田中, 厚成ほか

Publisher: 航空宇宙技術研究所

Publication date: 1991-12

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: When aero-engines are developed, several different types of wind tunnel tests are involved. For instance, one type of tunnel is required for fundament...

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 Institutional Repositories DataBase(IRDB)(Institutional Repository) is linked at the site of Institutional Repositories DataBase(IRDB)(Institutional Repository).
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: IHI航空エンジンにおける風洞実験とCFD
Author/Editor: 田中, 厚成
Tanaka, Atsushige
Author Heading: 田中, 厚成
Tanaka, Atsushige
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1991-12
Publication Date (W3CDTF): 1991-12
Alternative Title: Role of Wind Tunnel Tests and CFD Analysis for the Development of Aero-Engines in IHI
Periodical title: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-16
No. or year of volume/issue: 16
Volume: 16
Pages: 337-344
ISSN (Periodical Title): ISSN : 0289-260X
Text Language Code: jpn
Target Audience: 一般
Note (General): When aero-engines are developed, several different types of wind tunnel tests are involved. For instance, one type of tunnel is required for fundamental tests of the cascades; a second is required for high altitude engine performance tests. Experimental models for these tests consist of real engine components or of close replicas. Certain effects may not be adequately addressed in wind tunnel tests, for example, the effects of high speed revolution, flow properties in unmeasurable regions, realistic boundary conditions. The twofold object of computational fluid dynamics (CFD) for internal flows is to predict the performance of models before expensive wind tunnel tests are done and to provide information of the internal flow that is inaccessible to experiment measurement. CFD is already useful for improving designs or making new ones. As computers and CFD technology advance, CFD can expand from the role of prediction and design to that of a numerical wind tunnel. This paper shows how features of numerical wind tunnels parallel those of experimental wind tunnels The paper also assesses future trends for the use of numerical wind tunnels.
資料番号: NALSP0016053
レポート番号: NAL SP-16
Access Restrictions: 限定公開
Periodical Title (NCID): AN10097345
https://ci.nii.ac.jp/ncid/AN10097345
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