TRAIL - Technical Report Archive and Image Library

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

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

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

The Design of Airplane-Engine Superchargers

Full-scale wind-tunnel and flight test of a Fairchild 22 airplane equipped with a Zap flap and Zap ailerons

Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps

Performance Characteristics of Venturi Tubes Used in Aircraft for Operating Air-Driven Gyroscopic Instruments

Effect of Air-Entry Angle on Performance of a 2-Stroke-Cycle Compression-Ignition Engine

Bending Tests of Circular Cylinders of Corrugated Aluminum-Alloy Sheet

Full-Scale Wind-Tunnel and Flight Tests of a Fairchild 22 Airplane Equipped With External-Airfoil Flaps

Fuselage-drag tests in the variable-density wind tunnel: streamline bodies of revolution, fineness ratio of 5

Free spinning wind-tunnel tests of a low-wing monoplane with systematic wings and tails 2: Mass distributed along the fuselage

Free-spinning wind-tunnel tests of a low-wing monoplane with systemic changes in wings and tails 1: Basic loading condition

Full scale span load distribution on a tapered wing with split flaps of various spans

Discharge characteristics of a double injection-valve single-pump injection system

Tank tests of two models of flying-boat hulls to determine the effect of ventilating the step

Theoretical span loading and moments of tapered wings produced by aileron deflection

Compression-ignition engine performance at altitudes and at various air pressures and temperatures

Charts expressing the time, velocity, and altitude relations for an airplane diving in a standard atmosphere

The measurement of air speed in airplanes

Wind-tunnel tests of a Clark Y wing with "Maxwell" leading-edge slots

Energy Loss, Velocity Distribution, and Temperature Distribution for a Baffled Cylinder Model

Empirical corrections to the span load distribution at the tip

Heat transfer from cylinders having closely spaced fins

Spinning characteristics of wings 4: changes in stagger of rectangular Clark Y cellules

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