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• The Calculation of Wing Float Displacement in Single-Float Seaplanes
• The Estimation of Airplane Performance From Wind Tunnel Tests on Conventional Airplane Models
• The Velocity Distribution Caused by an Airplane at the Points of a Vertical Plane Containing the Span
• Model Tests on the Economy and Effectiveness of Helicopter Propellers
• Pressure Distribution on the Nose of an Airship in Circling Flight
• The Drift of an Aircraft Guided Towards Its Destination by Directional Receiving of Radio Signals Transmitted From the Ground
• Determination of the Lift and Drag Characteristics of an Airplane in Flight
• The Flettner Rotor Ship in the Light of the Kutta-Joukowski Theory and of Experimental Results
• Propeller Scale Effect and Body Interference
• Wind Tunnel Tests of Fuselages and Windshields
• Two-Stroke-Cycle Engines for Airplanes
• The fundamental principles of high-speed semi-diesel engines. Part 3: a discussion of fuel mixing and ignition, with special reference to engines with precombustion chambers
• The fundamental principles of high-speed semi-diesel engines. Part 1: a general discussion of the subject of fuel injection in diesel engines and detailed descriptions of many types of injection nozzles
• The fundamental principles of high-speed semi-diesel engines. Part 2: a discussion of the semi-diesel principle and its application to various types of solid-injection engines
• Investigation of turbulence in wind tunnels by a study of the flow about cylinders
• Heinkel airplane H.D. 39 for carrying newspapers
• Air force and moment for N-20 wing with certain cut-outs
• The air forces on a model of the sperry messenger airplane without propeller
• Aerodynamic characteristics of airfoils IV : continuation of reports nos. 93, 124, and 182
• Behm acoustic sounder for aircraft
• The Blackburn "Sprat": A Training Airplane Convertible into Landplane or Seaplane
• Standard atmosphere - tables and data
• Protection of wooden airplane parts against moisture by means of varnish
• Tests for determining the effect of a rotating cylinder fitted into the leading edge of an airplane wing
• Pressure distribution over thick tapered airfoils, NACA 81, USA 27c modified and USA 35
• Spray penetration with a simple fuel injection nozzle
• Stability Equations for Airship Hulls
• A study of the effect of a diving start on airplane speed
• Comparison of tests on air propellers in flight with wind tunnel model tests on similar forms
• An investigation of the coefficient of discharge of liquids through small round orifices
• Tests on an airfoil with two slots suitable for an aircraft of high performance : lift, drag, rolling and yawing moment measurements
• The Belgian Aerotechnical Laboratory at Rhode-Saint-Genese
• The Pander light biplane : a school two-seater with 45 HP Anzani engine
• Liore-Olivier airplane : type 12 night-bomber or type 20 commercial
• Slip Stream Effect
• The New De Havilland Commercial Airplane: The D.H. 66 With Three Bristol "Jupiter" Engines
• Preliminary Wing Model Tests in the Variable Density Wind Tunnel of the National Advisory Committee for Aeronautics
• Fuels for High-Compression Engines
• Determining Size of Drops in Fuel Mixture of Internal Combustion Engines
• Experiments With a Sphere From Which the Boundary Layer Is Removed by Suction
• Experiments on Autorotation
• Flight Tests on Airplanes
• Experiments With Rotating Cylinders in Combination With Airfoils
• All-Metal Junkers Airplane, Type F 13
• The Albatros L 72A: A German Newspaper Carrier With Slotted Wings
• Calculation of Combining Effects in the Structure of Airplane Wings: A Rational Basis for Estimating the Reduction in the Design Load on Wing Beams Due to the Influence of Ribs and Covering Toward Causing the Beams to Deflect Together
• The Bristol "Badminton" Airplane
• Cooling of Air-Cooled Engines by Forced Circulation of Air
• Two 'Gloster' Airplanes: The 'Grouse II,' - Two-Seat Training Airplane, The 'Grebe II,' Single-Seat Fighter
• Mixing and Ignition in Supercharged Engines