%0 Generic %A Loftin, Laurence K , Jr, %T Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6). %U http://hdl.handle.net/2060/19930083926