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• Notes on Propeller Design 1: The Energy Losses of the Propeller
• Notes on Propeller Design III: The Aerodynamical Equations of the Propeller Blade Elements
• Full Scale Determination of the Lift and Drag of a Seaplane
• Notes on Propeller Design 2:The Distribution of Thrust Over a Propeller Blade
• The Choice of the Speed of an Airship
• Stresses Produced on an Airship Flying Through Gusty Air
• Notes on Aerodynamic Forces 3: The Aerodynamic Forces on Airships
• The twisted wing with elliptic plan form
• Notes on Aerodynamic Forces I: Rectilinear Motion
• Notes on Aerodynamic Forces 2: Curvilinear Motion
• Notes on Propeller Design 4: General Proceeding in Design
• Wind-Driven Propellers (Or "Windmills")
• Wind Tunnel of Zeppelin Airship Company
• Some New Aerodynamical Relations
• The Drag of Zeppelin Airships
• General Biplane Theory
• General Theory of Thin Wing Sections
• The Tail Plane
• The Minimum Induced Drag of Aerofoils
• The Determination of the Angles of Attack of Zero Lift and of Zero Moment, Based on Munk's Integrals
• Analysis of Dr. Schaffran's Propeller Model Tests
• General Theory of Windmills
• Reduction in Efficiency of Propellers Due to Slipstream
• The analysis of free flight propeller tests and its application to design
• Analysis of W. F. Durand's and E. P. Lesley's propeller tests
• Remarks on the Pressure Distribution over the Surface of an Ellipsoid, Moving Translationally Through a Perfect Fluid
• The Aerodynamic Forces on Airship Hulls
• Note on the Pressure Distribution Over the Hull of Elongated Airships With Circular Cross Section
• Note on the Relative Effect of the Dihedral and the Sweep Back of Airplane Wings
• Some Tables of the Factor of Apparent Additional Mass
• On the Distribution of Lift Along the Span of an Airfoil With Displaced Ailerons
• Remarks on the Pressure Distribution over the Surface of an Ellipsoid, Moving Translationally Through a Perfect Fluid
• Comparing the Performance of Geometrically Similar Airplanes
• Note on Vortices on Their Relation to the Lift of Airfoils
• The Induction Factor Used for Computing the Rolling Moment Due to the Ailerons
• The Simplifying Assumptions, Reducing the Strict Application of Classical Hydrodynamics to Practical Aeronautical Computations
• Note on the Air Forces on a Wing Caused by Pitching.
• Determination and Classification of the Aerodynamic Properties of Wing Sections
• A New Relation Between the Induced Yawing Moment and the Rolling Moment of an Airfoil in Straight Motion
• Model Tests With a Systematic Series of 27 Wing Sections at Full Reynolds Number
• Elements of the Wing Section Theory and of the Wing Theory
• Elements of the Wing Section Theory and of the Wing Theory
• The Velocity Distribution Caused by an Airplane at the Points of a Vertical Plane Containing the Span
• Model Tests on the Economy and Effectiveness of Helicopter Propellers
• The air forces on a model of the sperry messenger airplane without propeller
• Preliminary Wing Model Tests in the Variable Density Wind Tunnel of the National Advisory Committee for Aeronautics
• The Variable Density Wind Tunnel of the National Advisory Committee for Aeronautics
• The Spacing of Orifices for the Measure of Pressure Distributions
• The air forces on a systematic series of biplane and triplane cellule models
• The aerodynamic characteristics of seven frequently used wing sections at full Reynolds number