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Direct-reading design charts for 24S-T3 aluminum-alloy flat compression panels having longitudinal formed hat-section stiffeners and comparisons with panels having z-section stiffeners
- Author / Creator
- Available as
- Online
- Summary
-
Direct-reading design charts are presented for 24S-T3 aluminum-alloy flat compression panels having longitudinal formed hat-section stiffeners. These charts make possible the direct determination o...
Direct-reading design charts are presented for 24S-T3 aluminum-alloy flat compression panels having longitudinal formed hat-section stiffeners. These charts make possible the direct determination of the stress and all panel proportions required to carry a given intensity of loading with a given skin thickness and effective length of panel. A comparison is made of the relative merits of hat- and Z-stiffened covers of box beams which are subjected to compression plus bending and to compression pluse bending plus vertical shear.
Details
- Creator
- by William A. Hickman and Norris F. Dow
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1953
- Physical Details
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- 1 online resource (71 pages) : illustrations, tables, photographs
- data file
- OCLC
- on1353819268
- Date of issue: March 1953.
- "Langley Aeronautical Laboratory.⁰́₊
- Title from title screen (viewed December 5, 2022)
- Report no. NACA-TN-2792.
- Includes bibliographical references (pages 19-20)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.