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Effect of Horizontal-tail Span and Vertical Location on the Aerodynamic Characteristics of an Unswept Tail Assembly in Sideslip
Donald R. Riley
出版National Advisory Committee for Aeronautics, 1953
URLhttp://books.google.com.hk/books?id=lde4v3EnS0sC&hl=&source=gbs_api
EBookFULL_PUBLIC_DOMAIN
註釋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.