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NACA-TR-827
Charts for the minimum-weight design of 24s-t aluminum-alloy flat compression panels with longitudinal z-section stiffeners
Year: 1945
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.
Subject: ALLOYS
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:34:58Z | |
| date available | 2017-09-04T16:34:58Z | |
| date copyright | 01/01/1945 | |
| date issued | 1945 | |
| identifier other | UYWUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/98511 | |
| description 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. | |
| language | English | |
| title | NACA-TR-827 | num |
| title | Charts for the minimum-weight design of 24s-t aluminum-alloy flat compression panels with longitudinal z-section stiffeners | en |
| type | standard | |
| page | 28 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1945 | |
| contenttype | fulltext | |
| subject keywords | ALLOYS | |
| subject keywords | ALUMINUM | |
| subject keywords | BUCKLING | |
| subject keywords | CHARTS | |
| subject keywords | COMPRESSION | |
| subject keywords | COMPRESSIVE | |
| subject keywords | DESIGN | |
| subject keywords | FLAT | |
| subject keywords | LOADS | |
| subject keywords | PANELS | |
| subject keywords | PLATES | |
| subject keywords | REINFORCED | |
| subject keywords | SKIN | |
| subject keywords | STIFFENING | |
| subject keywords | STRENGTH | |
| subject keywords | STRESSED | |
| subject keywords | STRUCTURES |