DESIGN CHARTS for Longitudinally Stiffened Wing Compression Panels

490182

01/01/1949

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
THE problems encountered in the design of longitudinally stiffened wing compression panels are summarized, and the extensive experimental investigations of the strength of such panels conducted by the NACA are reviewed.
The development of design charts, based on the test data obtained in these investigations is described, and the importance of the proper selection of parameters for the chart is emphasized.
Several illustrative examples are presented to show how the most suitable panel proportions for a particular application may be selected from the charts.
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DOI
https://doi.org/10.4271/490182
Pages
23
Citation
DOW, N., "DESIGN CHARTS for Longitudinally Stiffened Wing Compression Panels," SAE Technical Paper 490182, 1949, https://doi.org/10.4271/490182.
Additional Details
Publisher
Published
Jan 1, 1949
Product Code
490182
Content Type
Technical Paper
Language
English