Low-speed Wind-tunnel Investigation of a Thin 60 Degree Delta Wing with Double Slotted, Single Slotted, Plain, and Split Flaps

Report presenting a low-speed wind-tunnel investigation to determine the longitudinal aerodynamic characteristics of a thin delta wing equipped with various arrangements of double slotted, single slotted, plain, and split flaps. The wing was a flat plate with beveled leading and trailing edges and had a maximum thickness ratio of 0.045, and 60 degrees sweepback of the leading edge.