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• The Effect of Wind Tunnel Turbulence Upon the Forces Measured on Models
• The Induction Factor Used for Computing the Rolling Moment Due to the Ailerons
• Structural Weight of Aircraft as Affected by the System of Design
• The Logarithmic Polar Curve - Its Theory and Application to the Predetermination of Airplane Performance
• The Simplifying Assumptions, Reducing the Strict Application of Classical Hydrodynamics to Practical Aeronautical Computations
• The Testing of Aviation Engines Under Approximate Altitude Conditions
• Tests of rotating cylinders
• The influence of inlet air temperature and jacket water temperature on initiating combustion in a high speed compression ignition engine
• Tests on Duralumin Columns for Aircraft Construction
• Nonmetallic diaphragms for instruments
• Interference tests on NACA pitot tubes
• Flame speed and spark intensity
• Air forces on airfoils moving faster than sound
• Aerodynamic characteristics of airfoils at high speeds
• Airplane parachutes
• Standardization tests of NACA no. 1 wind tunnel
• Altitude of equilibrium of an airship
• Aeronautic instruments. Section 1: general classification of instruments and problems including bibliography
• Preliminary investigation of the effect of a rotating cylinder in a wing
• The effects of shielding the tips of airfoils
• The application of propeller test data to design and performance calculations
• The sparking voltage of spark plugs
• Recent experiments at the Gottingen Aerodynamic Institute
• Charts for graphical estimation of airplane performance
• Note on the Air Forces on a Wing Caused by Pitching.
• Determination and Classification of the Aerodynamic Properties of Wing Sections
• Results of Recent Experiments With Slotted Wings
• Experimental Determination of Pressure Drop Caused by Wire Gauze in an Air Stream
• Hulls for Large Seaplanes
• Royal Aero Club Light Aeroplane Competition
• Some Problems on the Lift and Rolling Moment of Airplane Wings
• The "Navigraph"
• Investigation of Slipstream Velocity
• Latécoère Air Lines
• Relation Of "Lilienthal Effect" to Dynamic Soaring Flight
• The Problem of Fuel Measurement: The Schiske "Konsummeter"
• A New Relation Between the Induced Yawing Moment and the Rolling Moment of an Airfoil in Straight Motion
• Law of Similitude for the Surface Resistance of Lacquered Planes Moving in a Straight Line Through Water
• The Effect of Changes in Compression Ratio Upon Engine Performance
• European Commercial Aeronautics
• Alloys Similar to Duralumin Made in Other Countries Than Germany
• Potential Flow in Engine Valves
• Light Airplanes of France, Germany, Italy, Belgium, Holland, Czechoslovakia and Lithuania
• Effect of Speed on Economy of Airship Traffic
• Model Tests With a Systematic Series of 27 Wing Sections at Full Reynolds Number
• Increasing the Power of Internal Combustion Engines
• Correcting Horsepower Measurements to a Standard Temperature
• Computation of Cantilever Airplane Wings
• Pressure Distribution Over the Wings of an MB-3 Airplane in Flight
• Calculation of Wing Spars of Variable Cross-Section and Linear Load