Browse TRAIL Inventories

Drop and Flight Tests on NY-2 Landing Gears Including Measurements of Vertical Velocities at Landing

Annual Report of the National Advisory Committee for Aeronautics (16th). Administrative Report Including Technical Reports Nos. 337 to 364

The 7 by 10 Foot Wind Tunnel of the National Advisory Committee for Aeronautics

The Design and Development of an Automatic Injection Valve With an Annular Orifice of Varying Area

Mechanical Similitude and Turbulence

Definition of Method of Measurement of Supporting and Control Surface Areas

Airplane Landing Gear

Method of Determining the Weights of the Most Important Simple Girders

Wind Tunnel of the Bucharest Polytechnic Institute

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

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"

Experiments with planing surfaces

Airplane stability in taxying

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

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

General Potential Theory of Arbitrary Wing Sections

Reduction of Wing Lift by the Drag

Statistics of the Bureau Veritas

The Characteristics of a Clark Y Wing Model Equipped With Several Forms of Low-Drag Fixed Slots

Preliminary Investigation of Modifications to Conventional Airplanes to Give Nonstalling and Short-Landing Characteristics

The Automotive Ignition Coil

Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack 3: Ordinary Ailerons Rigged Up 10 Degrees When Neutral

Wind-Tunnel Tests of a Clark Y Wing With a Narrow Auxiliary Airfoil in Different Positions

Wing Characteristics as Affected by Protuberances of Short Span

The Mechanism of Atomization Accompanying Solid Injection

Measurement of the Differential and Total Thrust and Torque of Six Full-Scale Adjustable-Pitch Propellers

The Messerschmidt M.29 Touring Airplane (German): A Two-Seat Cantilever Monoplane

Problems Concerning the Stability and Maneuverability of Airplanes

Accurate Calculation of Multispar Cantilever and Semicantilever Wings With Parallel Webs Under Direct and Indirect Loading

Twelfth Rhon Soaring Contest, 1931

The Mutual Action of Airplane Body and Power Plant

Dynamic Testing of Airplane Shock-Absorbing Struts


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