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Works by Mary Jackson

namemediatypedateAuthorLanguagetypeNarrative locationTitle
Czarnecki, K. R.; Jackson, Mary W. (septiembre1958), Effects of Nose Angle and Mach Number on Transition on Cones at Supersonic Speeds (NACA TN 4388), National Advisory Committee for Aeronautics1958Mary Jackson
Jackson, Mary W.; Czarnecki, K.R. (1960), Investigation by Schlieren Technique of Methods of Fixing Fully Turbulent Flow on Models at Supersonic Speeds,1960Mary Jackson
Czarnecki, K. R.; Jackson, Mary W. (enero 1961), Effects of Cone Angle, Mach Number, and Nose Blunting on Transition at Supersonic Speeds (NASA TN D-634), NASA Langley Research Center1961Mary Jackson
Jackson, Mary W.; Czarnecki, K. R. (julio 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 Center1961Mary Jackson
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)1963Mary Jackson
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