Compression Buckling Analysis of Flat Panels with Z-section Stiffeners-Reference-Cited by-同舟云学术

Compression Buckling Analysis of Flat Panels with Z-section Stiffeners

Published:2017 Issue:3 Volume:60 Page:171-180
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

TAKI Toshimi¹

Affiliation:

1. Aerospace Company, Kawasaki Heavy Industries, Ltd.

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/60/3/60_T-16-51/_pdf

Reference18 articles.

1. 1) Hickman, W. A. and Dow, N. F.: Data on the Compressive Strength of 75S-T6 Aluminum-Alloy Flat Panels with Longitudinal Extruded Z-Section Stiffeners, NACA TN-1829, 1949.

2. 2) Hickman, W. A. and Dow, N. F.: Data on the Compressive Strength of 75S-T6 Aluminum-Alloy Flat Panels Having Small, Thin, Widely Spaced, Longitudinal Extruded Z-Section Stiffeners, NACA TN-1978, 1949.

3. 3) Semonian, J. W. and Peterson, J. P.: An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-Stringer Panels with Special Reference to the Influence of Riveted Connection between Sheet and Stringer, NACA TN-3431, 1955.

4. 4) Schuette, E. H.: Charts for the Minimum-Weight Design of 24S-T Aluminum-Alloy Flat Compression Panels with Longitudinal Z-section Stiffeners, NACA ARR No. L5F15, 1945.

5. 5) Hickman, W. A. and Dow, N.: Direct-Reading Design Charts for 75S-T6 Aluminum-Alloy Flat Compression Panels Having Longitudinal Extruded Z-section Stiffeners, NACA TN-2435, 1952.

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1. Optimization of Flat Z-stiffened Panel Subjected to Compression;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2019