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Lateral-directional stability characteristics of a wing-fuselage configuration at angles of attack up to 44 deg (1974)

Huffman, J. K. ; Henderson, W. P.

In: CASI

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Publication Date: 2019-06-27

Description: An investigation has been conducted to determine the effects of configuration variables on the lateral-directional stability characteristics of a wing-fuselage configuration. The variables under study included variations in the location of a single center-line vertical tail and twin vertical tails, wing height, fuselage strakes, and horizontal tails. The study was conducted in the Langley high-speed 7-by 10-foot tunnel at a Mach number of 0.30, at angles of attack up to 44 deg and at sideslip angles of 0 deg and plus or minus 5 deg.

Keywords: AERODYNAMICS

Type: NASA-TM-X-3087 , L-9541

Format: application/pdf

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