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- Wind-Tunnel Investigation of Control-Surface Characteristics 21: Medium and Large Aerodynamic Balances of Two Nose Shapes and a Plain Overhang Used With a 0.40-Airfoil-Chord Flap on an NACA 0009 Airfoil
- Wind-Tunnel Investigation of Control-Surface Characteristics 22: Medium and Large Aerodynamic Balances of Two Nose Shapes and a Plain Overhang Used With a 0.20-Airfoil-Chord Flap on an NACA 0009 Airfoil
- Effect of Aerodynamic Refinement on the Aerodynamic Characteristics of a Flying-Boat Hull
- Aerodynamic Characteristics of Three Deep-Stepped Planing-Tail Flying-Boat Hulls
- Aerodynamic Characteristics of Flying-Boat Hulls Having Length-Beam Ratios of 20 and 30
- High-Speed Wind-Tunnel Investigation of a Flying-Boat Hull With High Length-Beam Ratio
- Preliminary Aerodynamic Investigation of the Effect of Camber on a 60 Degree Delta Wing with Round and Beveled Leading Edges
- Preliminary Wind-Tunnel Investigation at High-Subsonic Speeds of Planing-Tail, Blended, and Airfoil-Forebody Swept Hulls
- Transonic Stability and Control Investigation of a 1/80-Scale Model of the Consolidated Vultee Skate 9 Seaplane, TED No. NACA DE 345: Transonic-Bump Method
- The Effect of End Plates on Swept Wings at Low Speed
- Stability and control characteristics at low speed of a 1/5-scale model of the Edo 142 hydro-ski research airplane
- Aerodynamic Characteristics of a Flying-Boat Hull Having a Length-Beam Ratio of 15, TED No. NACA 2206
- Aerodynamic Characteristics of a Refined Deep-Step Planing-Tail Flying-Boat Hull with Various Forebody and Afterbody Shapes
- Aerodynamic Characteristics of Three Deep-Step Planing-Tail Flying-Boat Hulls and a Transverse-Step Hull with Extended Afterbody
- Low-Speed Investigation of the Effects of Location of a Delta and a Straight Tail on the Longitudinal Stability and Control of a Thin Delta Wing With Extended Double Slotted Flaps
- A Correlation of Two-Dimensional Data on Lift Coefficient Available With Blowing-, Suction-, Slotted-, and Plain-Flap High-Lift Devices
- Low-speed static stability characteristics of a cambered-delta-wing model
- Wind-tunnel investigation of jet-augmented flaps on a rectangular wing to high momentum coefficients
- Exploratory wind-tunnel investigation to determine the lift effects of blowing over flaps from nacelles mounted above the wing