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• Conversion of Energy in Cross-Sectional Divergences Under Different Conditions of Inflow
• Torsional Stresses in Box Beams With Cross Sections Partially Restrained Against Warping
• Effect of Fuselage and Engine Nacelles on Some Aerodynamic Properties of an Airplane Wing
• Contribution to the Mutual Interference of Wing and Propeller
• Infrared Radiation From Explosions in a Spark-Ignition Engine
• The drag of airplane wheels, wheel fairings, and landing gears - 1
• The Weathering of Aluminum Alloy Sheet Materials Used in Aircraft
• The Effect of Spray Strips on the Take-Off Performance of a Model of a Flying-Boat Hull
• Potential Flow About Elongated Bodies of Revolution
• Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack 12: Upper-Surface Ailerons on Wings With Split Flaps
• Scale Effect on Clark Y Airfoil Characteristics From NACA Full-Scale Wind-Tunnel Tests
• Some Factors Affecting Combustion in an Internal-Combustion Engine
• A Flight Investigation of the Effect of Mass Distribution and Control Setting on the Spinning of the XN2Y-1 Airplane
• Tests of Nacelle-Propeller Combinations in Various Positions with Reference to Wings 5: Clark Y Biplane Cellule - NACA Cowled Nacelle - Tractor Propeller
• An Analysis of Longitudinal Stability in Power-Off Flight With Charts for Use in Design
• Analysis of 2-Spar Cantilever Wings With Special Reference to Torsion and Load Transference
• The Short "Scylla" Commercial Airplane (British): An All-Metal Biplane
• The British Klemm "Eagle" Commercial Airplane: A Low-Wing Cantilever Monoplane
• The De Havilland "Comet" Long-Range Airplane (British): A Low-Wing Cantilever Monoplane
• Avro 642 Commercial Airplane (British): A High-Wing Cantilever Monoplane
• The Avro "Commodore" Touring Airplane (British): A Cabin Biplane
• The Avia 51 Commercial Airplane (Czechoslovakian): A Cantilever High-Wing Monoplane
• Fokker F.XX Commercial Airplane (Dutch): A High-Wing Cantilever Monoplane
• The Comper "Streak" Single Seat Airplane (British): A Low-Wing Cantilever Monoplane
• D.H. 86 "Express Air Liner" (British): A Four-Engine Biplane
• General Theory of Aerodynamic Instability and the Mechanism of Flutter
• Resume of Present Data on Load Distribution on Slots and Flaps, Special Report
• Preliminary Wind-Tunnel and Flight Tests of a Balanced Split Flap, Special Report
• Wing-Nacelle-Propeller Tests - Comparative Tests of Liquid-Cooled and Air-Cooled Engine Nacelles
• Additional Test Data on Static Longitudinal Stability
• Paris Aviation Salon, 1934
• Investigation of boundary layers on an airplane wing in free flight
• Avro C.30 Direct-Control Autogiro (British)
• Annual Report of the National Advisory Committee for Aeronautics (19th). Administrative Report Including Technical Report Nos. 441 to 474
• Improved Apparatus for the Measurement of Fluctuations of Air Speed in Turbulent Flow
• On the Theory of Laminar Boundary Layers Involving Separation
• General equations for the stress analysis of rings
• Full-scale wind-tunnel tests of a PCA-2 autogiro rotor
• The drag of airplane wheels, wheel fairings, and landing gears - 3
• The effect of baffles on the temperature distribution and heat-transfer coefficients of finned cylinders
• The drag of airplane wheels, wheel fairings, and landing gears 2: nonretractable and partly retractable landing gears
• A comparison of fuel sprays from several types of injection nozzles
• A description and test results of a spark-ignition and a compression-ignition 2-stroke-cycle engine
• Tests of nacelle-propeller combinations in various positions with reference to wings 6: wings and nacelles with pusher propeller
• Cooling characteristics of a 2-row radial engine
• Wind-tunnel research comparing lateral control devices particularly at high angles of attack 13: auxiliary airfoils used as external ailerons
• The influence of tip shape on the wing load distribution as determined by flight tests
• The influence of wing setting on the wing load and rotor speed of a PCA-2 autogiro as determined in flight
• Spinning characteristics of wings 1: rectangular Clark Y monoplane wing
• An Aerodynamic Analysis of the Autogiro Rotor With a Comparison Between Calculated and Experimental Results