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• The Drag of Streamline Wires
• Future problems of soaring flight : report of 1932 Rhon soaring contest
• Aerodynamic forces and moments of a seaplane on the water
• An airfoil spanning an open jet
• Scale effect of model in seaplane-float investigations
• Heinkel He 64 C sport airplane (German) : a two-seat low-wing cantilever monoplane
• The aerodynamic forces and moments exerted on a spinning model of the NY-1 airplane as measured by the spinning balance
• Aircraft speed instruments
• The effect of multiple fixed slots and a trailing-edge flap on the lift and drag of a Clark Y airfoil
• The experimental determination of the moments of inertia of airplanes
• Wind-tunnel research comparing lateral control devices, particularly at high angles of attack V : spoilers and ailerons on rectangular wings
• The physical effects of detonation in a closed cylindrical chamber
• Ice prevention on aircraft by means of engine exhaust heat and a technical study of heat transmission from a Clark y airfoil
• The Hanriot-Biche 110 C1 airplane (French) : an all-metal low-wing pursuit monoplane
• The Airspeed "Courier" commercial airplane (British) : a low-wing cantilever monoplane
• The Caudron P.V. 200 touring airplane (French) : an all-metal amphibian monoplane
• Tests for the Elimination of Tail Flutter
• A Simple Method for Increasing the Lift of Airplane Wings by Means of Flaps
• Pressure and Frictional Resistance of a Cylinder at Reynolds Numbers 5,000 to 40,000
• The Problem of the Propeller in Yaw With Special Reference to Airplane Stability
• Results of Extended Tests of the Focke-Wulf F 19a "Ente," a Tail-First Airplane
• Experiments With Needle Bearings
• Flight-Test Data on the Static Fore-and-Aft Stability of Various German Airplanes
• The D.V.L. Gliding-Angle Control (W. Hübner Design)
• Increasing the Volumetric Efficiency of Diesel Engines by Intake Pipes
• The Effect of a Gap Between Elevator and Stabilizer on the Static Stability and Maneuverability About the Lateral Axis in Flight
• Determination of Inherent Stresses by Measuring Deformations of Drilled Holes
• The Critical Shear Load of Rectangular Plates
• Development of the Rules Governing the Strength of Airplanes Part 1: German Loading Conditions Up to 1926
• Development of the Rules Governing the Strength of Airplanes Part 2: Loading Conditions in Germany (Continued), England and the United States
• Practical Experiences With Lightning Discharges to Airplanes
• Trend of Airplane Flight Characteristics
• The Theory of the Strandgren Cyclogyro
• Take-Off and Propeller Thrust
• Pressure Rise, Gas Vibrations and Combustion Noises During the Explosion of Fuels
• The Schneider Trophy Contest
• Knowledge Gained From Practical Experience in the Designing of Aircraft Engines
• Dynamic Breaking Tests of Airplane Parts
• Dimensions of Twin Seaplane Floats
• The N.A.C.A. Tank: A High-Speed Towing Basin for Testing Models of Seaplane Floats
• The N.A.C.A. High-Speed Wind Tunnel and Tests of Six Propeller Sections
• Interference on an Airfoil of Finite Span in an Open Wind Tunnel
• The Process of Separation in the Turbulent Friction Layer
• Effect of Viscosity on Fuel Leakage Between Lapped Plungers and Sleeves and on the Discharge From a Pump-Injection System
• Experimental Verification of the Theory of Wind-Tunnel Boundary Interference
• Strength Tests of Thin-Walled Duralumin Cylinders in Compression
• Wind-Tunnel Tests on Combinations of a Wing With Fixed Auxiliary Airfoils Having Various Chords and Profiles
• Wing-Fuselage Interference, Tail Buffeting, and Air Flow About the Tail of a Low-Wing Monoplane
• Aircraft Power-Plant Instruments
• The Westland "Wallace" General-Purpose Airplane (British): An All-Metal Biplane