The Effects of Changes in Aspect Ratio and Tail Height on the Longitudinal Stability Characteristics at High Subsonic Speeds of a Model With a Wing Having 32.6 Degree Sweepback
Description:
Report discussing an investigation to determine the effects of changes in aspect ratio and tail height on the longitudinal stability characteristics of a model with a 32.6-degree sweptback wing. The effects of a leading-edge discontinuity were also examined.
Date:
February 2, 1954
Creator:
Alford, William J., Jr. & Pasteur, Thomas B., Jr.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department