Effect of Horizontal-tail Span and Vertical Location on the Aerodynamic Characteristics of an Unswept Tail Assembly in Sideslip
Auteur : Donald R. Riley
Date de publication : 1953
Éditeur : National Advisory Committee for Aeronautics
Nombre de pages : 39
Résumé du livre
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.