Browse TRAIL Inventories

A Study of Curvilinear Flight

Static Longitudinal Stability Of "Ente" Airplanes

Investigation of Certain Wing Shapes With Sections Varying Progressively Along the Span

The Dangerous Sideslip of a Stalled Airplane and Its Prevention

The Dangerous Flat Spin and the Factors Affecting It

Determination of Resistance and Trimming Moment of Planing Water Craft

Elmira Soaring Contest, 1930

Eleventh Rhön Soaring-Flight Contest, 1930

The Use of Elektron Metal in Airplane Construction

On Floats and Float Tests

Clerget 100 Hp Heavy-Oil Engine

Spatial Buckling of Various Types of Airplane Strut Systems

Lift Distribution and Longitudinal Stability of an Airplane

Measurements of Vertical Air Currents in the Atmosphere

The Amiot 140 M Military Airplane (French): An All-Metal Multiplace High-Wing Monoplane

Breguet 390 T Commercial Airplane (French): A Ten-Seat All-Steel Sesquiplane

Breguet Military Airplane, Type 33: A Two-Place Long-Distance Sesquiplane for Observation and Bombing

The Mono-Spar Light Airplane (British): A Twin-Engined Low-Wing Cabin Monoplane

The Mureaux 111 R.2 Military Airplane (French): A Long-Distance All-Metal Observation Monoplane

Polish P Type Single-Seat Fighters: All-Metal Gull-Type Wing Monoplanes

The Dewoitine D.30 Commercial Airplane (French): A High-Wing Cantilever Monoplane

The Dewoitine D 33 Commercial Airplane (French): A Low-Wing Cantilever Monoplane

The Guilleman J.G. 10 (French) : A Two-Place Touring Low-Wing Monoplane

The Mauboussin M 11 Touring Airplane (French): A Two-Place High-Wing Monoplane

The Use of Slots for Increasing the Lift of Airplane Wings

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

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

Airship Model Tests in the Variable Density Wind Tunnel

Span-load distribution as a factor in stability in roll

The drag characteristics of several airships determined by deceleration tests

Tests of nacelle-propeller combinations in various positions with reference to wings. Part I : thick wing-N.A.C.A. cowled nacelle-tractor propeller

The effect of increased carburetor pressure on engine performance at several compression ratios

Effect of orifice length-diameter ratio on fuel sprays for compression-ignition engines

The effect on airplane performance of the factors that must be considered in applying low-drag cowling to radial engines

Pressure distribution tests on a series of Clark Y biplane cellules with special reference to stability

A method for computing leading-edge loads

The vertical wind tunnel of the National Advisory Committee for Aeronautics

Focke-Wulf F 19a "Ente" Commercial Airplane (German): A Tail-First High-Wing Monoplane

The Aerodynamic Wind Vane and the Inherent Stability of Airplanes

Downwash Measurements Behind Wings With Detached Float

The New "Charlestop" Remote Brake Transmission and Control

Optico-Photographic Measurements of Airplane Deformations

Combined Pitching and Yawing Motion of Airplanes


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