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• Wind-Tunnel Tests on a Series of Wing Models Through a Large Angle of Attack Range Part 1: Force Tests
• The Cierva "Autogiro" Mark III (British): Armstrong-Siddeley "Genet Major" Engine
• Pressure Distribution Over a Thick, Tapered and Twisted Monoplane Wing Model-N.A.C.A. 81-J
• Strength of Welded Joints in Tubular Members for Aircraft
• Impact Tests on Rubber Compression Springs for Airplane Landing Gears
• Load Assumptions for Calculating the Strength of Airplanes
• Effects of the End Fixation of Airplane Struts
• Flight Tests for the Determination of Static Longitudinal Stability
• Balanced and Servo Control Surfaces
• Combating Airplane Fires
• A Possible Method for Preventing the Autorotation of Airplane Wings
• Experimental Investigations Concerning the Limits of Detonation in Gaseous Mixtures: Part 1
• Experimental Research on the Friction of Pivots
• "Gloster" Metal Construction
• Contribution to the Study of Normal Burning in Gaseous Carbureted Mixtures: Part 1
• English Airplane Construction
• Structural Details of the Giant Dornier Seaplane "Do X."
• Structural Details of German Light Airplanes
• Göttingen Six-Component Scale Measurements on a Junkers A 35 Airplane Model
• Coefficients of Flow of Standard Nozzles
• Diesel-Engine Investigations: Ignition-Chamber Engines
• Relation Between the Stability Characteristics and the Controllability of German Airplanes
• The Relation Between the Tensile Strength and the Hardness of Metals
• The Electrodynamometric Balance of the Small Wind Tunnel of the French Service of Aeronautical Research
• The Short "Valetta" Commercial Seaplane (British): A High-Wing All-Metal Twin-Float Monoplane
• The Wibault 220 R.N. 3 Airplane (French): A Three-Place Observation High-Wing Monoplane
• Westland "Wessex" Commercial Airplane (British): A High-Wing Semicantilever Monoplane
• The "Potez 39" Observation Airplane (French): An All-Metal High-Wing Two-Seat Monoplane
• The "Avro Trainer" Airplane (British): A Training Biplane
• The De Havilland "Moth Three" Airplane (British): A High-Wing Commercial Monoplane
• The Boundary Layer as a Means of Controlling the Flow of Liquids and Gases
• The Farman "F.300" Commercial Airplane (French): A High-Wing Semicantilever Monoplane
• The Comper C(La)7 "Swift" Airplane (English): A High-Wing Single-Seat Monoplane
• Vickers "Viastra I" Commercial Airplane (British): A High-Wing All-Metal Semicantilever Monoplane
• Identification of Aircraft Tubing by Rockwell Test
• Static, Drop, and Flight Tests on Musselman Type Airwheels
• Aerodynamic Characteristics of Twenty-Four Airfoils at High Speeds
• Tests of Five Metal Model Propellers With Various Pitch Distributions in a Free Wind Stream and in Combination With Model VE-7 Fuselage
• Annual Report of the National Advisory Committee for Aeronautics (15th). Administrative Report Including Technical Reports Nos. 309 to 336
• Fuel Vapor Pressures and the Relation of Vapor Pressure to the Preparation of Fuel for Combustion in Fuel Injection Engines
• Airfoil Pressure Distribution Investigation in the Variable Density Wind Tunnel
• Full-scale tests of metal propellers at high tip speeds
• Coefficients of discharge of fuel-injection nozzles for compression-ignition engines
• Comparative flight performance with an NACA Roots supercharger and a turbocentrifugal supercharger
• Comparison of full-scale propellers having R.A.F.-6 and Clark Y airfoil sections
• Maneuverability investigation of the F6C-3 airplane with special flight instruments
• Experimental determination of jet boundary corrections for airfoil tests in four open wind tunnel jets of different shapes
• Pressure distribution over a symmetrical airfoil section with trailing edge flap
• Pressure distribution over the fuselage of a PW-9 pursuit airplane in flight
• Maneuverability investigation of an F6C-4 fighting airplane