Flight Test of Stable Automated Cruise Flap for an Adaptive Wing Aircraft

0p-optimization function was effective in producing pressure differentials that would have reduced drag. The effectivenessoftheC 0 p-maintenancefunctioncouldnotbedeterminedbecauseoflargesample-to-samplevariations in measured C 0 p values. It remains unknown whether this high-frequency content actually represented rapidly varying pressures on the airfoil surface or if it was the result of noise in the measurement system.