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• Riveted Joints in Thin Plates
• The Behm acoustic sounder for airplanes with reference to its accuracy
• Flow and Force Equations for a Body Revolving in a Fluid
• The measurement of fluctuations of air speed by the hot-wire anemometer
• Dynamic and flight tests on rubber-cord and oleo-rubber-disk landing gears for an F6C-4 airplane
• Air forces and air-force moments at large angles of attack and how they are affected by the shape of the wing
• Aerodynamic characteristics of airfoils VI : continuation of reports nos. 93, 124, 182, 244, and 286
• Effect of variation of chord and span of ailerons on hinge moments at several angles of pitch
• A method of flight measurement of spins
• Pressure element of constant logarithmic stiffness for temperature compensated altimeter
• The effect of supercharger capacity on engine and airplane performance
• Joint report on standardization tests on N.P.L. R.A.F 15 airfoil model
• Collection of wind-tunnel data on commonly used wing sections
• Flight tests on U.S.S. Los Angeles. Part 2: stress and strength determination
• Investigation of the variations in the velocity of the air flow about a wing profile
• Mathematical treatise on the recovery from a flat spin
• The "Latecoere 28" commercial airplane (French) : a ten passenger high-wing monoplane
• The Liore Olivier "Le 0.240" commercial seaplane (French) : a high-wing cantilever monoplane
• The Handley Page type 42 commercial airplane (British) : a metal sesquiplane
• The Henderson "Hendy" 302 cabin airplane (British) : a two-seat low-wing cantilever monoplane
• The Dornier "Do.X" flying boat (German) : a giant high-wing monoplane
• The Dyle and Bacalan "D.B. 80" day mail airplane (French) : an all-metal high-wing monoplane
• The Dyle and Bacalan "DB 70" commercial airplane (French) : an all-metal high-wing monoplane
• The Caproni "90 P.B." military airplane (Italian) : a giant biplane of 6000 horsepower
• The "Comte A.C. 3" military airplane (Swiss) : a high-wing semicantilever monoplane
• Measurement of Profile Drag on an Airplane in Flight by the Momentum Method: Part 2
• Measurement of Profile Drag on an Airplane in Flight by the Momentum Method: Part 1
• Propulsion by Reaction
• Determination of the Maximum Control Forces and Attainable Quickness in the Operation of Airplane Controls
• Calculation of Tapered Monoplane Wings
• Calculation of Pressure Distribution on Airship Hulls
• Experimental Investigations Concerning the Limits of Detonation in Gaseous Mixtures: Part 2
• Improving the Performance of Multi-Engined Airplanes by Means of Idling Propellers: The "Free-Wheel" Propeller
• Determination of the Best Cross Section for a Box Beam Subjected to Bending Stresses
• Counter-Propeller
• Contribution to the Theory of Propeller Vibrations
• Development of the Junkers-Diesel Aircraft Engine
• Experimental Investigation of Aircraft Propellers Exposed to Oblique Air Currents
• Practical Tests With The "Auto Control Slot" Part 2: Discussion
• Theory of the Landing Impact of Seaplanes
• Ratier Metal Propeller With Pitch Variable in Flight
• Practical Tests With The "Auto Control Slot" Part 1: Lecture
• Contribution to the Study of Normal Burning in Gaseous Carbureted Mixtures: Part 2
• Riveting in Metal Airplane Construction Part 4: Strength of Riveted Joints in Duralumin (Concluded), Comparative Tests With Riveted Joints
• Riveting in Metal Airplane Construction Part 2: Riveting Methods and Equipment (Concluded), Strength of Riveted Joints in Duralumin
• Riveting in Metal Airplane Construction Part 3: Strength of Riveted Joints in Duralumin (Continued), Test Installation and Arrangement
• The Magnus Effect in Theory and in Reality
• Recent Tests of Tailless Airplanes
• Metal Covering of Airplanes
• Present Status of Aircraft Instruments