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- Nonstationary flow about a wing-aileron-tab combination including aerodynamic balance
- Flutter calculations in three degrees of freedom
- Preliminary vibration and flutter studies on P-47 tail
- Vibration Surveys of the P-47-B Rudder and Fin-Rudder Assembly
- Vibration Surveys of the P-40 Rudder and Fin-Rudder Assembly
- Flutter tests of modified SB2U model in 16-foot tunnel
- Flutter tests on SB2U model in 16-foot tunnel
- Airfoil-contour modifications based on (epsilon)-curve method of calculating pressure distribution
- The Theory of Propellers 4: Thrust, Energy, and Efficiency Formulas for Single- and Dual-Rotating Propellers With Ideal Circulation Distribution
- The Theory of Propellers 1: Determination of the Circulation Function and the Mass Coefficient for Dual-Rotating Propellers
- The Theory of Propellers 3: The Slipstream Contraction With Numerical Values for Two-Blade and Four-Blade Propellers
- The Theory of Propellers 4: Thrust, Energy, and Efficiency Formulas for Single and Dual Rotating Propellers With Ideal Circulation Distribution
- The Theory of Propellers 3: The Slipstream Contraction With Numerical Values for Two-Blade and Four-Blade Propeller
- The Theory of Propellers 2: Method for Calculating the Axial Interference Velocity
- The Theory of Propellers 2: Method for Calculating the Axial Interference Velocity
- The Theory of Propellers 1: Determination of the Circulation Function and the Mass Coefficient for Dual-Rotating Propellers
- Effect of a Trailing-Edge Extension on the Characteristics of a Propeller Section
- Vibration-Response Tests of a 1/5-Scale Model of the Grumman F6F Airplane in the Langley 16-Foot High-Speed Tunnel
- Experiments on Drag of Revolving Disks, Cylinders, and Streamline Rods at High Speeds
- Effect of the Lift Coefficient on Propeller Flutter
- Note on the Theorems of Bjerknes and Crocco
- Pressure Distributions for Representative Airfoils and Related Profiles
- A Condition on the Initial Shock
- Extension of the Chaplygin Proofs on the Existence of Compressible-Flow Solutions to the Supersonic Region
- The Problem of Noise Reduction With Reference to Light Airplanes
- General Theory of Aerodynamic Instability and the Mechanism of Flutter