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- Sideslip angles and vertical-tail loads in rolling pull-out maneuvers
- Voltera's Solution of the Wave Equation as Applied to Three-Dimensional Supersonic Airfoil Problems
- Sideslip Angles and Vertical-Tail Loads Developed by Periodic Control Deflections
- Downwash in the vertical and horizontal planes of symmetry behind a triangular wing in supersonic flow
- Linearized compressible-flow theory for sonic flight speeds
- Formulas for source, doublet, and vortex distributions in supersonic wing theory
- The calculation of downwash behind supersonic wings with an application to triangular plan forms
- Linearized compressible-flow theory for sonic flight speeds
- The Indicial Lift and Pitching Moment for a Sinking or Pitching Two-Dimensional Wing Flying at Subsonic or Supersonic Speeds
- Generalized conical-flow fields in supersonic wing theory
- Theoretical aerodynamic characteristics of a family of slender wing-tail-body combinations
- Integrals and integral equations in linearized wing theory
- Two-and three-dimensional unsteady lift problems in high-speed flight
- Chordwise and Compressibility Corrections to Slender-Wing Theory
- Generalized indicial forces on deforming rectangular wings in supersonic flight
- Lift Developed on Unrestrained Rectangular Wings Entering Gusts at Subsonic and Supersonic Speeds
- Generalized indical forces on deforming rectangular wings in supersonic flight
- A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds
- Nonlifting Wing-Body Combinations With Certain Geometric Restraints Having Minimum Wave Drag at Low Supersonic Speeds
- The Wave Drag of Arbitrary Configurations in Linearized Flow as Determined by Areas and Forces in Oblique Planes
- A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds
- Wing-Body Combinations With Certain Geometric Restraints Having Low Zero-Lift Wave Drag at Low Supersonic Mach Numbers
- A method for the calculation of wave drag on supersonic-edged wings and biplanes