Study made of 2 methods proposed to reduce high sinking speeds and improve landing characteristics of low aspect ratio hypersonic aircraft by placing wing at large angles of sideslip to increase its effective aspect ratio; summary of results obtained.
Low-speed investigation of effects of large wing-sideslip angles on aerodynamic characteristics of two arrow-wing -- Fuselage arrangements
NASA -- Tech Note
1961
41 pages
Report
Englisch
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