Charts for the minimum-weight design of the 24S-T aluminum-alloy flat compression panels with longitudinal Z-section stiffeners / by Evan H. Schuette.
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| Main Author: | |
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| Corporate Authors: | , |
| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1945]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L197. |
| Subjects: |
| Abstract: | Design charts are developed for 24S-T aluminum-alloy flat compression panels with longitudinal Z-section stiffeners. These charts make possible the design of the lightest panels of this type for a wide range of design requirements. Examples of the use of the charts are given and it is pointed out on the basis of these examples that, over a wide range of design conditions, the maintenance of buckle-free surfaces does not conflict with the achievement of high structural efficiency. The achievement of the maximum possible structural efficiency with 24S-T aluminum-alloy panels, however, requires closer stiffener spacings than those now in common use. |
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| Item Description: | NACA Wartime Report L-197. Originally issued as NACA as Advance Restricted Report L5F15 (August 1945) Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. |
| Physical Description: | 41 pages, 23 unnumbered pages : illustrations, tables ; 27 cm. |
| Bibliography: | Includes bibliographical references. |