Title: Investigation of Effect of Sideslip on Lateral Stability Characteristics II : Rectangular Midwing on Circular Fuselage with Variations in Vertical-tail Area and Fuselage Length with and Without Horizontal Tail Surface
Abstract: Report presenting power-off tests made in the 6- by 6-foot test section of the stability tunnel to determine the variation of the static lateral stability characteristics with vertical-tail area, fuselage length, and wing dihedral. The results are presented as curves showing the variation of the static-lateral-stability slopes with angle of attack, and the rolling-moment, yawing-moment, and lateral-force coefficients with angle of yaw.
Publication Year: 1945
Publication Date: 1945-04-01
Language: en
Type: article
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