Investigation of the Effect of Sweep on the Flutter of Cantilever Wings
Description:
Report presenting an experimental and analytical investigation of the flutter of uniform sweptback cantilever wings. The experiments used groups of wings sweptback by rotating and by shearing with angles of sweep ranging from 0 to 60 degrees. Results regarding the experimental investigation and a discussion and comparison of the analytical and experimental results are provided.
Date:
November 15, 1948
Creator:
Barmby, J. G.; Cunningham, H. J. & Garrick, I. E.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department