Experimental and Numerical Investigation of 65-deg Delta and 65/40-deg Double-Delta Wings in Sideslip
28th, AIAA Applied Aerodynamics Conference ; 2010 ; Chicago, Il
01.01.2010
13 pages
Aufsatz (Konferenz)
Englisch
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An experimental study of double delta wings in sideslip
AIAA | 1991
|Rolling moment due to sideslip of delta wings.
AIAA | 1967
|