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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


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