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- Divergence of swept wings
- Calculation of the aerodynamic loading of swept and unswept flexible wings of arbitrary stiffness
- A Simple Approximate Method for Obtaining Spanwise Lift Distributions Over Swept Wings
- Calculation of the Aerodynamic Loading of Flexible Wings of Arbitrary Plan Form and Stiffness
- Theoretical spanwise lift distributions of low-aspect-ratio wings at speeds below and above the speed of sound
- Approximate aerodynamic influence coefficients for wings of arbitrary plan form in subsonic flow
- Calculated Lift Distributions of a Consolidated Vultee B-36 and Two Boeing B-47 Airplanes Coupled at the Wing Tips
- Charts and tables for use in calculations of downwash of wings of arbitrary plan form
- A plan-form parameter for correlating certain aerodynamic characteristics of swept wings
- Calculation of the lateral control of swept and unswept flexible wings of arbitrary stiffness
- Calculated Aerodynamic Loadings of M, W, and Delta Wings in Incompressible Flow
- A Simple Approximate Method for Calculating Spanwise Lift Distributions and Aerodynamic Influence Coefficients
- The Calculation of Certain Static Aeroelastic Phenomena of Wings With Tip Tanks or Boom-Mounted Lifting Surfaces
- Calculated spanwise lift distributions and aerodynamic influence coefficients for unswept wings in subsonic flow
- Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings
- Calculated spanwise lift distributions, influence functions, and influence coefficients for unswept wings in subsonic flow
- Static aeroelastic phenomena of M-, W-, and A-wings
- Calculated spanwise lift distributions and aerodynamic influence coefficients for swept wings in subsonic flow
- The response of an airplane to random atmospheric disturbances
- Expected numbers of maxima and minima of a stationary random process with non-Gaussian frequency distribution
- The response of an airplane to random atmospheric disturbances
- Effect of spanwise variations in gust intensity on the lift due to atmospheric turbulence