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A Study of Transparent Plastics for use on Aircraft, Special Report

Supplement to A Study of Transparent Plastics for use on Aircraft

Stability of Castering Wheels for Aircraft Landing Gears, Special Report

Tests in the Variable-Density Tunnel of Seven Tapered Wings Having N.A.C.A. 230 Mean Lines, Special Report

Compressible Flow About Symmetrical Joukowski Profiles

Stress Analysis of Beams With Shear Deformation of the Flanges

Stability of Castering Wheels for Aircraft Landing Gears

The Hafner A.R. III Gyroplane (British)

Pressure Distribution Over Airfoils With Fowler Flaps

Drag of Cylinders of Simple Shapes

Baynes Bee Light Airplane (British): A Two-Seat High-Wing Monoplane

The Airspeed "Oxford" Training Airplane (British): A Two-Engine Cantilever Monoplane

Armstrong Whitworth 27 "Ensign" Commercial Airplane (British): An All-Metal High-Wing Monoplane

Fairey "Battle" Medium Bomber Airplane (British): An All-Metal Low-Wing Cantilever Monoplane

Experimental Apparatus for the Study of Propellers

Helicopter Problems

Turbulent Boundary Layer of an Airfoil

Universal Logarithmic Law of Velocity Distribution as Applied to the Investigation of Boundary Layer and Drag of Streamline Bodies at Large Reynolds Number

Detonation and Autoignition: Some Considerations on Methods of Determination

Contributions to the Theory of Incomplete Tension Bay

The Scale Effect in Towing Tests With Airplane-Float Systems

The Strength of Shell Bodies: Theory and Practice

Tapered Wings, Tip Stalling, and Preliminary Results From Tests of the Stall-Control Flap

The Stability of Orthotropic Elliptic Cylinders in Pure Bending

Charts for Checking the Stability of Plane Systems of Rods

Pressure Distribution on a Wing Section With Slotted Flap in Free Flight Tests

Wing-Fuselage Interference - Comparison of Conventional and Airfoil-Type-Fuselage Combinations

The Photoelastic Investigation of Three-Dimensional Stress and Strain Conditions

The Gyroplane: Its Principles and Its Possibilities

Ground Effect - Theory and Practice

On the Actual Loads on Airplane Landing Gears

Valve-Spring Surge

The Transition Phase in the Take-Off of an Airplane

Torsion Tests of Tubes

Column Strength of Tubes Elastically Restrained Against Rotation at the Ends

Wind-Tunnel Investigation of Tapered Wings With Ordinary Ailerons and Partial-Span Split Flaps

The Effect of Curvature on the Transition From Laminar to Turbulent Boundary Layer

Static Thrust Analysis of the Lifting Airscrew

A Sound Pressure-Level Meter Without Amplification

Motion of the Two-Control Airplane in Rectilinear Flight After Initial Disturbances With Introduction of Controls Following an Exponential Law

Pressure Drop in Tubing in Aircraft Instrument Installations

Stability of Structural Members Under Axial Load

Strain Measurements on Small Duralumin Box Beams in Bending

A Study of the Factors Affecting the Range of Airplanes

Pressure Distribution Over a Clark Y-H Airfoil Section With a Split Flap

Increasing the Strength of Aluminum-Alloy Columns by Prestressing

Noise From Propellers With Symmetrical Sections at Zero Blade Angle

The Source of Propeller Noise

Method of Curved Models and Its Application to the Study of Curvilinear Flight of Airships: Part 2

Method of Curved Models and Its Application to the Study of Curvilinear Flight of Airships: Part 1


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