%0 Generic %A Kehlet, Alan B, %T Free-flight Investigation over a Mach Number Range from 0.74 to 1.43 at Lift Coefficients from Minus 0.15 to 0.75 of an Airplane-configuration Model Having a 52.5 Degree Delta Wing and a Low Swept Horizontal Tail. %U http://hdl.handle.net/2060/19930089281