Browse TRAIL Inventories

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

Flat Sheet Metal Girders With Very Thin Metal Web. Part 1: General Theories and Assumptions

Experiments With a Wing From Which the Boundary Layer Is Removed by Suction

Flat Sheet Metal Girders With Very Thin Metal Web. Part 3: Sheet Metal Girders With Spars Resistant to Bending - the Stress in Uprights - Diagonal Tension Fields

Flat Sheet Metal Girders With Very Thin Metal Web. Part 2: Sheet Metal Girders With Spars Resistant to Bending - Oblique Uprights - Stiffness

Wrinkling Phenomena of Thin Flat Plates Subjected to Shear Stresses

Wrinkling of Reinforced Plates Subjected to Shear Stresses

The Steady Spin

Superchargers

Flutter in Propeller Blades

Development of a Non-Autorotative Airplane Capable of Steep Landing

On Atomization in Carburetors

Goldstein's Solution of the Problem of the Aircraft Propeller With a Finite Number of Blades

A New Principle of Sound Frequency Analysis

On the Theory of Wing Sections With Particular Reference to the Lift Distribution

Flame Movement and Pressure Development in an Engine Cylinder

Penetration and Duration of Fuel Sprays From a Pump Injection System

The NACA Apparatus for Studying the Formation and Combustion of Fuel Sprays and the Results From Preliminary Tests

Hydraulics of Fuel-Injection Pumps for Compression-Ignition Engines

The Oehmichen Peugeot Helicopter

Landing of Seaplanes

Load Assumptions for the Landing Impact of Seaplanes

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

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


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