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Direct-reading design charts for 75S-T6 aluminum-alloy flat compression panels having longitudinal extruded z-section stiffeners
- Author / Creator
- Available as
- Online
- Summary
-
Direct-reading design charts are presented for 75S-T6 aluminum-alloy flat compression panels having longitudinal extruded z-section stiffeners. These charts, which cover a wide range of proportions...
Direct-reading design charts are presented for 75S-T6 aluminum-alloy flat compression panels having longitudinal extruded z-section stiffeners. These charts, which cover a wide range of proportions, make possible the direct determination of the stress and all panel distributions required to carry a given intensity of loading with a given skin thickness and effective length of panel.
Details
- Creator
- William A. Hickman and Norris F. Dow
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1952
- Physical Details
-
- 1 online resource (60 pages) : illustrations, tables
- data file
- OCLC
- on1333704436
- "Langley Aeronautical Laboratory."
- Title from title screen (viewed June 28, 2022)
- Date of issue: February 1952.
- Report numbers NACA-TN-2435.
- Includes bibliographical references (page 10)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.