An Experimental Investigation of the Effects of Leading Edge Extensions and Forebody Flow Separators on the Forebody-Vortex Induced Aerodynamics of a Generic Fighter Configuration
9th Applied aerodynamics conference ; 1991 ; Baltimore; MD
1991-01-01
9 pages
In 2 vols; See also 6369.400F 1991 for papers 91-3201 - 91-3344 on fiche. See also 5066.100 vol 29 no 5 1992 for paper 91-3204. See also 4926.700 vol 30 no 3 1993 for selected papers
Conference paper
English
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