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Low-speed Pressure-distribution Investigation of a Thin-delta-wing--fuselage Model with Double Slotted Flap, Extended Double Slotted Flap, and Canard
Delwin R. Croom, Jarrett K. Huffman
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Abstract
Report presenting an investigation in the 300 mph 7- by 10-foot tunnel to determine the chordwise and spanwise load distribution on a thin 60 degree delta-wing-fuselage model equipped with double slotted and extended double slotted flaps. The effects of a canard on the loads of the wing with the extended double slotted flaps are also determined.