A Method of calculating the compressive strength of Z-stiffened panels that develop local instability - Info and Reading Options
By George L. Gallaher
"A Method of calculating the compressive strength of Z-stiffened panels that develop local instability" was published by National Advisory Committee for Aeronautics in 1947 - Washington, D.C, it has 15 pages and the language of the book is English.
“A Method of calculating the compressive strength of Z-stiffened panels that develop local instability” Metadata:
- Title: ➤ A Method of calculating the compressive strength of Z-stiffened panels that develop local instability
- Author: George L. Gallaher
- Language: English
- Number of Pages: 15
- Publisher: ➤ National Advisory Committee for Aeronautics
- Publish Date: 1947
- Publish Location: Washington, D.C
“A Method of calculating the compressive strength of Z-stiffened panels that develop local instability” Subjects and Themes:
- Subjects: ➤ Plates (Engineering) - Strains and stresses - Buckling (Mechanics) - Mathematical analysis - Plaques (Ingénierie) - Contraintes (Mécanique) - Flambage (Résistance des matériaux) - Analyse mathématique - Stress - Strain - Warping - Buckling
Edition Specifications:
- Pagination: 1 online resource (15 pages)
Edition Identifiers:
- The Open Library ID: OL44477741M - OL32663403W
- Online Computer Library Center (OCLC) ID: 919093676
- ISBN-13: 9781680156102
- ISBN-10: 1680156101
- All ISBNs: 1680156101 - 9781680156102
AI-generated Review of “A Method of calculating the compressive strength of Z-stiffened panels that develop local instability”:
"A Method of calculating the compressive strength of Z-stiffened panels that develop local instability" Description:
The Open Library:
A method, based on the elastic theory for plate buckling and test results for 24S-T aluminum-alloy Z-stiffened panels, is shown for calculating the compressive strength of Z-stiffened panels that develop local instability. This method can be used to calculate the critical compressive stress above, as well as within, the elastic range. For stresses above three-fourths the compressive yield stress the method can be used for the approximate determination of the average compressive stress at maximum load.
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