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• Working Charts for the Determination of the Lift Distribution Between Biplane Wings
• The Breguet 410 and 411 Military Airplanes (French): Multiplace Sesquiplane Fighters
• Supplement to the Supermarine S.6.B. Racing Seaplane (British): A Low-Wing Twin-Float Monoplane
• General Formulas and Charts for the Calculation of Airplane Performance
• The Characteristics of a Clark Y Wing Model Equipped With Several Forms of Low-Drag Fixed Slots
• Preliminary Investigation of Modifications to Conventional Airplanes to Give Nonstalling and Short-Landing Characteristics
• The Automotive Ignition Coil
• Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack 3: Ordinary Ailerons Rigged Up 10 Degrees When Neutral
• Wind-Tunnel Tests of a Clark Y Wing With a Narrow Auxiliary Airfoil in Different Positions
• Wing Characteristics as Affected by Protuberances of Short Span
• The Mechanism of Atomization Accompanying Solid Injection
• Measurement of the Differential and Total Thrust and Torque of Six Full-Scale Adjustable-Pitch Propellers
• The Messerschmidt M.29 Touring Airplane (German): A Two-Seat Cantilever Monoplane
• Problems Concerning the Stability and Maneuverability of Airplanes
• Accurate Calculation of Multispar Cantilever and Semicantilever Wings With Parallel Webs Under Direct and Indirect Loading
• Twelfth Rhon Soaring Contest, 1931
• The Mutual Action of Airplane Body and Power Plant
• Dynamic Testing of Airplane Shock-Absorbing Struts
• German Aircraft Accident Statistics, 1930
• Torsional Vibration of Aircraft Engines
• The Breda 32 Commercial Airplane (Italian): A Three-Engine All-Metal Low-Wing Monoplane
• The D.H. "Fox Moth" Commercial Airplane (British): A Three-Passenger Light Cabin Biplane
• The Avro 631 Training Airplane (British): A Two-Seat Light Biplane
• Armstrong-Whitworth A.W. 15 "Atlanta" Airplane (British): A Commercial Multiplace Cantilever Monoplane
• The Armstrong Whitworth A.W. 16 Military Airplane (British): A Single-Seat Biplane
• The Stieger ST. 4 Light Airplane (British): A Twin-Engine Four-Seat Low-Wing Cabin Monoplane
• The Farman Night Bombers 211 and 212 (French): Four-Engine High-Wing Monoplanes
• Spartan "Cruiser" Commercial Airplane (British): A Six-Seat Low-Wing Cantilever Monoplane
• General Potential Theory of Arbitrary Wing Sections
• Reduction of Wing Lift by the Drag
• Statistics of the Bureau Veritas
• Stresses Produced in Airplane Wings by Gusts
• Vertical Descent of the Autogiro
• The Effect of Humidity on Engine Power at Altitude
• Annual Report of the National Advisory Committee for Aeronautics (17th). Administrative Report Including Technical Report Nos. 365 to 400
• Rates of fuel discharge as affected by the design of fuel-injection systems for internal-combustion engines
• Fuel vaporization and its effect on combustion in a high-speed compression-ignition engine
• The drag of two streamline bodies as affected by protuberances and appendages
• Tests of nacelle-propeller combinations in various positions with reference to wings 2: thick wing - various radial-engine cowlings - tractor propeller
• Wind-tunnel research comparing lateral control devices, particularly at high angles of attack 4: floating tip ailerons on rectangular wings
• The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel
• Wind-tunnel research comparing lateral control devices, particularly at high angles of attack 6: skewed ailerons on rectangular wings
• Wind-tunnel research comparing lateral control devices, particularly at high angles of attack 2: slotted ailerons and frise ailerons
• Characteristics of Clark Y airfoils of small aspect ratios
• A flight investigation of the spinning of the NY-1 airplane with varied mass distribution and other modifications, and an analysis based on wind-tunnel tests
• Experiments on the distribution of fuel in fuel sprays
• Photomicrographic studies of fuel sprays
• Lift and drag characteristics and gliding performance of an autogiro as determined in flight
• The effect of nozzle design and operating conditions on the atomization and distribution of fuel sprays
• Development of Tailless and All-Wing Gliders and Airplanes