%0 Generic %A Czarnecki, K R, %E Sinclair, Archibald R, %T Investigation of Boundary-layer Transition on 10 Degree Cone in Langley 4- by 4-foot Supersonic Pressure Tunnel at Mach Numbers of 1.41, 1.61, and 2.01. %U http://hdl.handle.net/2060/19930084419