補強板の圧縮強度 | NDL Search

補強板の圧縮強度

Material type: 文書・図像類

Author: 三本木, 茂夫ほか

Publisher: 航空宇宙技術研究所

Publication date: 1980-09

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: The Compressive strength of flat stiffened panels is analysed and compared with experimental results. The elastic-plastis and geometric nonlinear anal...

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: 補強板の圧縮強度
Author/Editor: 三本木, 茂夫
SANBONGI, Shigeo
Author Heading: 三本木, 茂夫
SANBONGI, Shigeo
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1980-09
Publication Date (W3CDTF): 1980-09
Alternative Title: Compressive Strength of Flat Stiffened Panels
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-624
No. or year of volume/issue: 624
Volume: 624
Pages: 19-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): The Compressive strength of flat stiffened panels is analysed and compared with experimental results. The elastic-plastis and geometric nonlinear analysis by the finite element method is carried out for short-panels. An experiment on the monolithic stiffened panels and riveted panels is also conducted. These results are compared with the crippling strength computed by Gerard’s formula. For the panels of intermediate length, overall buckling stresses are analysed by the use of Johnson-Euler formula and the tangent modulus equation of column buckling, connected with nonlinear analysis. Computed results for the Z-section stiffened panels are compared with published test data.
資料番号: NALTR0624000
レポート番号: NAL TR-624
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44879&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44879&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