DPW-W1, W2

Geometry

• b = wing span = 1524. mm• Sref = reference area = 290.322 mm2

• AR = aspect ratio = b2/Sref = 8.0• L.E. sweep angle = 17.2 degrees• T.E. sweep angle = 15.0 degrees

Wing Flow Conditions

• M = inlet Mach number = 0.76– Compressible flow

• ReL = Reynolds number = 5,000,000– Turbulent flow

• = angle of attack = -1.0, 0.0, 0.5, 1.0, 1.5, 2.0, 2.5, 3.0

4

DPW3 – Wing Alone

5

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7

8

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