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- Wind tunnel tests of an NACA 23021 airfoil equipped with a slotted extensible and a plain extensible flap
- Wind-Tunnel Investigation of the Lift Characteristics of an NACA 27-212 Airfoil Equipped With Two Types of Flap, Special Report
- Wind-Tunnel Investigation of an NACA 23021 Airfoil With Two Sizes of Balanced Split Flaps
- Jet-Boundary Corrections to the Downwash Behind Powered Models in Rectangular Wind Tunnels With Numerical Values for 7- by 10-Foot Closed Wind Tunnels
- Determination of the Stability and Control Characteristics of Airplanes from Tests of Powered Models
- Jet-Boundary Corrections to a Yawed Model in a Closed Rectangular Wind Tunnel
- Jet-boundary corrections for reflection-plane models in rectangular wind tunnels
- Limitations of lifting-line theory for estimation of aileron hinge-moment characteristics
- Jet-boundary corrections for reflection-plane models in rectangular wind tunnels
- Wind-Tunnel Calibration and Correction Procedures for Three-Dimensional Models
- Lifting-Surface-Theory Values of the Damping in Roll and of the Parameter Used in Estimating Aileron Stick Forces
- An Electromagnetic-Analogy Method of Solving Lifting-Surface-Theory Problems
- A Lifting-Surface-Theory Solution and Tests of an Elliptic Tail Surface of Aspect Ratio 3 with a 0.5-Chord 0.85-Span Elevator
- Lifting-Surface-Theory Aspect-Ratio Corrections to the Lift and Hinge-Moment Parameters for Full-Span Elevators on Horizontal Tail Surfaces
- Lifting-Surface-Theory Aspect-Ratio Corrections to the Lift and Hinge-Moment Parameters for Full-Span Elevators on Horizontal Tail Surfaces