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- Effect of Mach and Reynolds Numbers on the Maximum Lift Coefficient Obtainable in Gradual and Abrupt Stalls of a Pursuit Airplane Equipped With a Low-Drag Wing
- Effect of Mach and Reynolds Numbers on Maximum Lift Coefficient
- Flight Observations of Aileron Flutter at High Mach Numbers as Affected by Several Modifications
- Aerodynamic Properties of Slender Wing-Body Combinations at Subsonic, Transonic, and Supersonic Speeds
- Aerodynamic Properties of Cruciform-Wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds
- On the Application of Transonic Similarity Rules
- On the Application of Transonic Similarity Rules to Wings of Finite Span
- Downwash and Sidewash Fields Behind Cruciform Wings
- Theoretical Prediction of Pressure Distributions on Nonlifting Airfoils at High Subsonic Speeds
- On the range of applicability of the transonic area rule
- On the Range of Applicability of the Transonic Area Rule
- Thin airfoil theory based on approximate solution of the transonic flow equation
