Publikacje Czarnecki, K. R.; Jackson, Mary W. (September 1958), Effects of Nose Angle and Mach Number on Transition on Cones at Supersonic Speeds (NACA TN 4388), National Advisory Committee for Aeronautics Jackson, Mary W.; Czarnecki, K.R. (1960), Investigation by Schlieren Technique of Methods of Fixing Fully Turbulent Flow on Models at Supersonic Speeds, 242, National Aeronautics and Space Administration Czarnecki, K. R.; Jackson, Mary W. (January 1961), Effects of Cone Angle, Mach Number, and Nose Blunting on Transition at Supersonic Speeds (NASA TN D-634), NASA Langley Research Center Jackson, Mary W.; Czarnecki, K. R. (July 1961), Boundary-Layer Transition on a Group of Blunt Nose Shapes at a Mach Number of 2.20 (NASA TN D-932), NASA Langley Research Center Czarnecki, K.R.; Jackson, Mary W.; Monta, William J. (1963), Studies of Skin Friction at Supersonic Speeds (Turbulent Boundary Layer and Skin Friction Data for Supersonic Transports) Jackson, Mary W.; Czarnecki, K. R.; Monta, William J. (July 1965), Turbulent Skin Friction at High Reynolds Numbers and Low Supersonic Velocities, National Aeronautics and Space Administration Czarnecki, K.R.; Jackson, M.W.;