Study made to determine effect of end plates on wing body combination with and without drooped chord extensions; results indicate that addition of plates to either wing slightly increased lift in low angle of attack, but slightly decreased lift at moderate and high angles.
Longitudinal aerodynamic characteristics of sweptback wing-body combination with and without end plates at mach numbers from 0.40 to 0.93
NASA -- Tech Note
1960
22 pages
Report
Englisch
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