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• The effect of small angles of yaw and pitch on the characteristics of airplane propellers
• Reduction of turbulence in wind tunnels
• Aeronautical education and research at the Swiss Institute of Technology in Zurich
• Latecoere 38-0 flying boat (French) : a long-range sesquiplane for carrying mail
• The Hanriot H 431 military airplane (French) : a general purpose biplane
• The "I.A.R." pursuit airplane (Roumanian) : a one-place cantilever low-wing monoplane
• The C.A.M.S. 60 seaplane (French) : a twin-engine bombing and torpedo monoplane
• The Bernard 80 G.R. long-distance airplane (French) : a two-place cantilever monoplane
• The Bernard 120 seaplane (French) : a 1400 hp single-seat monoplane racer
• The Bleriot 110 airplane (French) : a long-distance high-wing monoplane
• The Oehmichen Peugeot Helicopter
• Landing of Seaplanes
• Load Assumptions for the Landing Impact of Seaplanes
• Flat Sheet Metal Girders With Very Thin Metal Web. Part 1: General Theories and Assumptions
• Experiments With a Wing From Which the Boundary Layer Is Removed by Suction
• Flat Sheet Metal Girders With Very Thin Metal Web. Part 3: Sheet Metal Girders With Spars Resistant to Bending - the Stress in Uprights - Diagonal Tension Fields
• Flat Sheet Metal Girders With Very Thin Metal Web. Part 2: Sheet Metal Girders With Spars Resistant to Bending - Oblique Uprights - Stiffness
• Wrinkling Phenomena of Thin Flat Plates Subjected to Shear Stresses
• Wrinkling of Reinforced Plates Subjected to Shear Stresses
• The Steady Spin
• Superchargers
• Flutter in Propeller Blades
• Development of a Non-Autorotative Airplane Capable of Steep Landing
• On Atomization in Carburetors
• Goldstein's Solution of the Problem of the Aircraft Propeller With a Finite Number of Blades
• A New Principle of Sound Frequency Analysis
• On the Theory of Wing Sections With Particular Reference to the Lift Distribution
• Flame Movement and Pressure Development in an Engine Cylinder
• Penetration and Duration of Fuel Sprays From a Pump Injection System
• The NACA Apparatus for Studying the Formation and Combustion of Fuel Sprays and the Results From Preliminary Tests
• Hydraulics of Fuel-Injection Pumps for Compression-Ignition Engines
• Combustion in a High-Speed Compression-Ignition Engine
• Strength of Rectangular Flat Plates Under Edge Compression
• The Elimination of Fire Hazard Due to Back Fires
• The Avro 627 "Mailplane" (English): A Single-Seat Biplane
• The Theory of Wind-Tunnel Wall Interference
• Theory of Wing Sections of Arbitrary Shape
• Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack 1: Ordinary Ailerons on Rectangular Wings
• Investigation of the Diaphragm-Type Pressure Cell
• The Comparative Performance of Superchargers
• Resistance of Plates and Pipes at High Reynolds Numbers
• The Transference of Heat From a Hot Plate to an Air Stream
• Landing Impact of Seaplanes
• Liquid Cooling of Aircraft Engines
• Relations Between Ship Design and Seaplane Design
• Measurement of Visibility From the Pilot's Cockpit on Different Airplane Types
• The Frictionless Flow in the Region Around Two Circles
• Effect of Viscosity in Speed Measurements With Double-Throat Venturi Tubes
• Experiments With Airplane Brakes
• Fire Prevention on Aircraft