Consideration of relative merits of wing-tip fins and central vertical fins in their comparative contribution to static directional stability derivative, rotary damping in yaw, and side-force slope of tailless aircraft. Before Inst Aeronautical Sciences.
Theoretical principles of wing-tip fins for tailless airplanes and their practical application
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 13 , n 10
1946
12 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
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