Browse TRAIL Inventories

Experiments With an Airfoil Model on Which the Boundary Layers Are Controlled Without the Use of Supplementary Equipment

Effect of Orifice Length-Diameter Ratio on the Coefficient of Discharge of Fuel-Injection Nozzles

Development of an Impinging-Jet Fuel-Injection Valve Nozzle

Effect of High Air Velocities on the Distribution and Penetration of a Fuel Spray

An integrating manometer for use in wind tunnel pressure distribution measurements

A Suggested Method for Measuring Turbulence

Strength Tests on Paper Cylinder in Compression, Bending and Shear

Wind-Tunnel Tests on Airfoil Boundary Layer Control Using a Backward-Opening Slot (1931)

The Variation in Pressure in the Cabin of an Airplane in Flight

Experiments with planing surfaces

Airplane stability in taxying

The aerodynamic safety of airplanes

A new chart for estimating the absolute ceiling of an airplane

Measurements of flow in the boundary layer of a 1/40-scale model of the U. S. Airship "Akron"

The Dornier Do K commercial airplane (German) : a high-wing cantilever monoplane

The Dreieck I Tailless Airplane (German) : A Low-Wing Cantilever Monoplane

Aerodynamic characteristics of circular-arc airfoils at high speeds

A comparison between the theoretical and measured longitudinal stability characteristics of an airplane

The aerodynamic characteristics of a slotted Clark y wing as affected by the auxiliary airfoil position

The aerodynamic characteristics of eight very thick airfoils from tests in the variable density wind tunnel

Airfoil section characteristics as affected by protuberances

Some approximate equations for the standard atmosphere

Force measurements on a 1/40-scale model of the U. S. Airship "Akron"

Pressure-distribution measurements on the hull and fins of scale model of the U. S. Airship "Akron"

The effect of area aspect ratio on the yawing moments of rudders at large angles of pitch on three fuselages

Investigation of damping liquids for aircraft instruments : II

Airplane flight in the stratosphere

Nieuport-Delage 590 Military airplane (French) : a two-place high-wing cantilever monoplane

The Latecoere 501 commercial seaplane (French) : a three-engine metal sesquiplane

The Loire 11 colonial military airplane (French) : a high-wing semicantilever all-metal monoplane

The C.A.M.S. 80 amphibian (French) : an observation monoplane

The Bleriot 137 military airplane (French) : a twin-engine multiplace monoplane

The Boulton and Paul P.64 mail-carrier : a two-engine all-metal biplane

Drag Tests of 4/9-Scale Model Engine Nacelles With Various Cowlings

Some Ideas on Racing Seaplanes

Transmission of Heat From a Flat Plate to a Fluid Flowing at a High Velocity

Resonance Vibrations of Aircraft Propellers

The Problem of Tire Sizes for Airplane Wheels

Problems Involved in the Choice and Use of Materials in Airplane Construction

Propeller Tip Flutter

Determination of Stresses and Deformations of Aircraft Propellers

Experiments With Intubed Propellers

Further Flight Tests on the Effectiveness of Handley Page Automatic Control Slots

Calculation of Potential Flow Past Airship Bodies in Yaw

The Testing of Airplane Fabrics

Methods for Facilitating the Blind Landing of Airplanes

Methods of Recording Rapid Wind Changes

The German Investigation of the Accident at Meopham (England)

Increase in the Maximum Lift of an Airplane Wing Due to a Sudden Increase in Its Effective Angle of Attack Resulting From a Gust

Combustion of Gaseous Mixtures


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