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- Pressure-distribution investigation on an NACA 0009 airfoil with a 30-percent-chord plain flap and three tabs
- Pressure-distribution investigation of an NACA 0009 airfoil with an 80-percent-chord plain flap and three tabs
- Wind-tunnel investigation of two airfoils with 25-percent-chord Gwinn and plain flaps
- Determination of control-surface characteristics from NACA plain-flap and tab data
- Wind-Tunnel Investigation of Control-Surface Characteristics 3: A Small Aerodynamic Balance of Various Nose Shapes Used With a 30-Percent-Chord Flap on an NACA 0009 Airfoil
- Wind-Tunnel Investigation of Control-Surface Characteristics 4: A Medium Aerodynamic Balance of Various Nose Shapes Used With a 30-Percent-Chord Flap on an NACA 0009 Airfoil
- Wind-tunnel investigation of a section of the horizontal tail surface for the Bell XP-63 airplane
- Determination of control-surface characteristics from NACA plain-flap and tab data