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- The determination of downwash
- Notes on the standard atmosphere
- Simple formula for estimating airplane ceilings
- Notes on the construction and testing of model airplanes
- Effect of aerofoil aspect ratio on the slope of the lift curve
- The variation of aerofoil lift and drag coefficients with changes in size and speed
- Relative efficiency of direct and geared drive propellers
- Reliable formulae for estimating airplane performance and the effects of changes in weight, wing area, or power
- Engine performance and the determination of absolute ceiling
- The general efficiency curve for air propellers
- The application of propeller test data to design and performance calculations
- Charts for graphical estimation of airplane performance
- The Reduction of Airplane Flight Test Data to Standard Atmosphere Conditions
- Standard atmosphere - tables and data
- A study of the effect of a diving start on airplane speed
- The effect of flight path inclination on airplane velocity
- Tests on airplane fuselages, floats and hulls
- Three methods of calculating range and endurance of airplanes
- Two practical methods for the calculation of the horizontal tail area necessary for a statically stable airplane
- Reduction of observed airplane performance to standard conditions
- A new chart for estimating the absolute ceiling of an airplane
- Some approximate equations for the standard atmosphere
- The estimation of maximum load capacity of seaplanes and flying boats
- Static thrust of airplane propellers
- Relative loading on biplane wings
- The calculation of take-off run
- The application of basic data on planing surfaces to the design of flying-boat hulls
- Some fundamental considerations in regard to the use of power in landing an airplane
- The mean aerodynamic chord and the aerodynamic center of a tapered wing