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Re(1): Harrier GR7 Airfoil Data
Posted on July 14, 2004 at 10:44:55 PM by
"AIAA 77-607 The AV-8B Wing : Aerodynamic Concept and Design" gives the following:
For an AV8B with 4 pylons + 2 x 300 gall tanks, stall angle at 18 AOA, CL is 1.7. At 0 AOA, CL is just under 0.6.
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