Low-speed lateral control characteristics of an unswept wing with hexagonal airfoil sections and aspect ratio 4.0 at a Reynolds number of 6.2 x 10(exp 6)
Description:
Report presenting a lateral-control investigation in the 19-foot pressure tunnel of an unswept wing with 6-percent-thick hexagonal airfoil sections, aspect ratio 4.0, and taper ratio 0.625. The wing was mounted on a circular fuselage with a fineness ratio of 10 to 1.
Date:
March 20, 1953
Creator:
Hadaway, William M.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department