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Method of Calculating the Compressive Strength of Z-Stiffened Panels that Develop Local Instability / George L. Gallaher, Rolla B. Boughan.
- Format:
- Book
- Author/Creator:
- Gallaher, George L., author.
- Boughan, Rolla B., author.
- Series:
- Technical note (United States. National Advisory Committee for Aeronautics) ; 1482.
- NACA Technical Note ; 1482
- Language:
- English
- Subjects (All):
- Buckling (Mechanics).
- Physical Description:
- 1 online resource (15 pages) : illustrations.
- Other Title:
- Method of Calculating the Compressive Strength of Z-Stiffened Panels that Develop Local Instability
- Place of Publication:
- Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
- Summary:
- 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.
- Notes:
- Description based on publisher supplied metadata and other sources.
- Includes bibliographical references.
- ISBN:
- 1-68015-610-1
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