YS-11A-500/600型主翼疲れ試験Ⅰ.セーフライフ試験荷重と試験方式

Material type: 文書・図像類

Author: 竹内, 和之ほか

Publisher: 航空宇宙技術研究所

Publication date: 1971-07

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: I was required to perform the full-scale fatigue test(the safe-life and fail-safe tests) of YS-11-500/600 transport wing, because the maximum take-off...

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: YS-11A-500/600型主翼疲れ試験Ⅰ.セーフライフ試験荷重と試験方式
Author/Editor: 竹内, 和之
野原, 利雄
朝田, 洋雄
TAKEUCHI, Kazuyuki
NOHARA, Toshio
ASADA, Hiroo
Author Heading: 竹内, 和之
野原, 利雄
朝田, 洋雄
TAKEUCHI, Kazuyuki
NOHARA, Toshio
ASADA, Hiroo
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1971-07
Publication Date (W3CDTF): 1971-07
Alternative Title: Full-Scale Fatigue Test of YS-11A-500/600 Turboprop Transport Wing(I Safe-Life Fatigue Test Loads and Test Method)
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-241
No. or year of volume/issue: 241
Volume: 241
Pages: 23-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): I was required to perform the full-scale fatigue test(the safe-life and fail-safe tests) of YS-11-500/600 transport wing, because the maximum take-off weight of the aircraft was increased by 2.2 tons compared with the prototype and accordingly some strength members of the wing were re-designed. In order to perform the full-scale fatigue test, the safe-life fatigue loads and test method were investigated and the fatigue loads and program sequence of the test are decided were follows:(1)Gust loads, maneuver loads and ground-air-ground loads are taken into consideration as fatigue test loads. (2)The flight loads of one block corresponding to 100 flights are applied in an ascending-descending sequence in which ground-air-ground loads are inserted.
資料番号: NALTR0241000
レポート番号: NAL TR-241
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