Effect of Horizontal-tail Span and Vertical Location on the Aerodynamic Characteristics of an Unswept Tail Assembly in Sideslip
Donald R. Riley
Jan 1953 · National Advisory Committee for Aeronautics
Ebook
39
Pages
About this ebook
An investigation has been conducted in the Langley stability tunnel on a vertical-tail model with a stub fuselage in combination with various horizontal tails to determine the effect of horizontal-tail span and vertical location of the horizontal tail relative to the vertical tail on the aerodynamic characteristics of an unswept tail assembly in sideslip.
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