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- Contributions to the Theory of Incomplete Tension Bay
- The Scale Effect in Towing Tests With Airplane-Float Systems
- The Strength of Shell Bodies: Theory and Practice
- Tapered Wings, Tip Stalling, and Preliminary Results From Tests of the Stall-Control Flap
- The Stability of Orthotropic Elliptic Cylinders in Pure Bending
- Charts for Checking the Stability of Plane Systems of Rods
- Pressure Distribution on a Wing Section With Slotted Flap in Free Flight Tests
- Wing-Fuselage Interference - Comparison of Conventional and Airfoil-Type-Fuselage Combinations
- The Photoelastic Investigation of Three-Dimensional Stress and Strain Conditions
- The Gyroplane: Its Principles and Its Possibilities
- Ground Effect - Theory and Practice
- On the Actual Loads on Airplane Landing Gears
- Valve-Spring Surge
- The Transition Phase in the Take-Off of an Airplane
- Torsion Tests of Tubes
- Column Strength of Tubes Elastically Restrained Against Rotation at the Ends
- Wind-Tunnel Investigation of Tapered Wings With Ordinary Ailerons and Partial-Span Split Flaps
- Compressible Flow About Symmetrical Joukowski Profiles
- Stress Analysis of Beams With Shear Deformation of the Flanges
- Stability of Castering Wheels for Aircraft Landing Gears
- The Hafner A.R. III Gyroplane (British)
- Pressure Distribution Over Airfoils With Fowler Flaps
- Drag of Cylinders of Simple Shapes
- Baynes Bee Light Airplane (British): A Two-Seat High-Wing Monoplane
- The Airspeed "Oxford" Training Airplane (British): A Two-Engine Cantilever Monoplane
- Armstrong Whitworth 27 "Ensign" Commercial Airplane (British): An All-Metal High-Wing Monoplane
- Fairey "Battle" Medium Bomber Airplane (British): An All-Metal Low-Wing Cantilever Monoplane
- The Effect of Curvature on the Transition From Laminar to Turbulent Boundary Layer
- The Design of Airplane-Engine Superchargers
- Full-scale wind-tunnel and flight test of a Fairchild 22 airplane equipped with a Zap flap and Zap ailerons
- Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps
- Performance Characteristics of Venturi Tubes Used in Aircraft for Operating Air-Driven Gyroscopic Instruments
- Effect of Air-Entry Angle on Performance of a 2-Stroke-Cycle Compression-Ignition Engine
- Bending Tests of Circular Cylinders of Corrugated Aluminum-Alloy Sheet
- Full-Scale Wind-Tunnel and Flight Tests of a Fairchild 22 Airplane Equipped With External-Airfoil Flaps
- Fuselage-drag tests in the variable-density wind tunnel: streamline bodies of revolution, fineness ratio of 5
- Free spinning wind-tunnel tests of a low-wing monoplane with systematic wings and tails 2: Mass distributed along the fuselage
- Free-spinning wind-tunnel tests of a low-wing monoplane with systemic changes in wings and tails 1: Basic loading condition
- Full scale span load distribution on a tapered wing with split flaps of various spans
- Discharge characteristics of a double injection-valve single-pump injection system
- Tank tests of two models of flying-boat hulls to determine the effect of ventilating the step
- Theoretical span loading and moments of tapered wings produced by aileron deflection
- Compression-ignition engine performance at altitudes and at various air pressures and temperatures
- Charts expressing the time, velocity, and altitude relations for an airplane diving in a standard atmosphere
- The measurement of air speed in airplanes
- Wind-tunnel tests of a Clark Y wing with "Maxwell" leading-edge slots
- Energy Loss, Velocity Distribution, and Temperature Distribution for a Baffled Cylinder Model
- Empirical corrections to the span load distribution at the tip
- Heat transfer from cylinders having closely spaced fins
- Spinning characteristics of wings 4: changes in stagger of rectangular Clark Y cellules