Additional comparisons between computed and measured transonic drag-rise coefficients at zero lift for wing-body-tail configurations
Description:
From Introduction: "This report makes further comparisons of the theoretical computing method with available experimental results, showing effects of wing plan-form changes, and the effect of an airfoil-section change on a wing of given plan form."
Date:
August 15, 1955
Creator:
Holdaway, George H.
Item Type:
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Partner:
UNT Libraries Government Documents Department