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Lateral-directional stability characteristics of a wing-fuselage configuration at angles of attack up to 44 degAn 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.
Document ID
19740023308
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Henderson, W. P. (NASA Langley Research Center Hampton, VA, United States)
Huffman, J. K. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Aerodynamics
Report/Patent Number
L-9541
NASA-TM-X-3087
Accession Number
74N31421
Funding Number(s)
PROJECT: RTOP 501-06-05-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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