Browse TRAIL Inventories

Effect of Developed Width on Strength of Axially Loaded Curved Sheet Stringer Panels

Investigation of the Behavior of Parallel Two-Dimensional Air Jets

An Investigation of the Characteristics of Alcohol-Distribution Tubes Used for Ice Protection on Aircraft Windshields

Wind-Tunnel Investigation of a 1/20-Scale Powered Model of a Four-Engine Transport Airplane

Performance of NACA Eight-Stage Axial-Flow Compressor at Simulated Altitudes

Performance Characteristics of Journal Bearings With Forced-Feed Lubrication

An Experimental Investigation of the Thrust and Torque Produced by Propellers Used as Aerodynamic Brakes

Investigation of Effect of Sideslip on Lateral Stability Characteristics 1: Circular Fuselage with Variations in Vertical-Tail Area and Tail Length With and Without Horizontal Tail Surface

High Temperature Characteristics of 17 Alloys at 1200 and 1350 Degrees F

The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA Free-Flight Tunnel

Effect of a Trailing-Edge Extension on the Characteristics of a Propeller Section

Simple Curves for Determining the Effects of Compressibility on Pressure Drop Through Radiators

High-Altitude Cooling 3: Radiators

Effect of Fuel Volatility on Performance of a Wright R-2600-8 Engine as Influenced by Mixture Distribution

Wind-Tunnel Investigation of Carburetor Air Scoops for the XTB2D-1 Airplane with Emphasis on Means for Bypassing the Boundary Layer

Wind-Tunnel Investigation of Ailerons on a Low-Drag Airfoil 3: The Effect of Tabs

The Effect of Engine Conditions on the Lead Susceptibility of Paraffinic Fuels

Experimental Study of the Coating Found on Scuffed Cast-Iron Piston Rings During Operation in Nitrided-Steel Cylinders

Wind-Tunnel Investigation of a Beveled Aileron Shape Designed to Increase the Useful Deflection Range

Tests of NACA 65(216)-420 and 66(218)-420 Airfoils at High Speeds

Cylinder-Head Cooling by Means of a Shield in the Exhaust Passage

Air-Consumption Parameters for Automatic Mixture Control of Aircraft Engines

Determination of the Stresses Produced by the Landing Impact in the Bulkheads of a Seaplane Bottom

Comparative Results of Tests on Several Different Types of Nozzles

Compressibility Effects on Heat Transfer and Pressure Drop in Smooth Cylindrical Tubes

Determination of the Actual Contact Surface of a Brush Contact

DVL Angular Velocity Recorder

Simply Supported Long Rectangular Plate Under Combined Axial Load and Normal Pressure

On the General Theory of Thin Airfoils for Nonuniform Motion

The "Limiting Line" in Mixed Subsonic and Supersonic Flow of Compressible Fluids

Dynamics of the Inlet System of a Four-Stroke Engine

Flight Investigation of Boundary-Layer Control by Suction Slots on an NACA 35-215 Low-Drag Airfoil at High Reynolds Numbers

Investigation of the Behavior of Parallel Two-Dimensional Air Jets

Simplified Truss Stability Criteria

Torsion Test to Failure of a Monocoque Box

Tests of Airfoils Designed to Delay the Compressibility Burble

The Effect of Temperature on Sheet Metals for Airplane Firewalls

The Influence of Plastic Deformation and of Heat Treatment on Poisson's Ratio for 18:8 Chromium-Nickel Steel

Plastic Mountings for Aircraft Windshields

Axial Fatigue of 10 Airplane Wing-Beam Specimens by the Resonance Method

Normal Pressure Tests on Unstiffened Flat Plates

An Interim Report on the Stability and Control of Tailless Airplanes

Protection of Nonmetallic Aircraft From Lightning 3: Electrical Effects in Glider Towlines

The Inward Bulge Type Buckling of Monocoque Cylinders 2: Experimental Investigation of the Buckling in Combined Bending and Compression

Aerodynamic Tests of a Full-Scale TBF-1 Aileron Installation in the Langley 16-Foot High-Speed Tunnel

Design of power-plant installations pressure-loss characteristics of duct components

Wind-Tunnel Procedure for Determination of Critical Stability and Control Characteristics of Airplanes

Tests of a Thermal Ice-Prevention System for a Wing Leading-Edge Landing-Light Installation

Application of Spring Tabs to Elevator Controls

A Theoretical Investigation of Longitudinal Stability of Airplanes with Free Controls Including Effect of Friction in Control System


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