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DESIGN CHARTS for Longitudinally Stiffened Wing Compression Panels

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Dow, Norris F., author.
Conference Name:
SAE National Aeronautic and Air Transport Meeting
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1949
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
490182
Access Restriction:
Restricted for use by site license

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