Investigation to determine wing surface pressures and aerodynamic loading associated with deflection of flap; data are presented for flap angles to 16° at Mach of 0.60 to 0.90 with R of 3.2 million and at Mach of 0.25 with R of 15.0 million.
Effects of inverse-taper leading-edge flap on aerodynamic loading characteristics of 45° sweptback wing at Mach numbers to 0.90
NASA -- Tech Note
1959
108 pages
Report
Englisch
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