Browse TRAIL Inventories

Flight Investigation of the Effects of Ice on an I-16 Jet-Propulsion Engine

Flight Tests of a Curtiss No. 838-1C2-18 Three-Blade Propeller Having Trailing-Edge Extensions

Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the McDonnell XP-88 Airplane with a Conventional Tail

Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the McDonnell XP-88 Airplane with a Vee Tail

The High-Speed Longitudinal Stability and Control of the Bell P-39N-1 Airplane as Calculated from Propeller-Off Tests of a 0.35-Scale Model

The High-Speed Longitudinal Stability and Control of the Bell P-39N-1 Airplane as Calculated from Propeller-Off Tests of a 0.35-Scale Model

High-Speed Aerodynamic Characteristics of a 1/7-Scale Model of the Northrop YB-49 Airplane

Estimated Flying Qualities of the Martin Model 202 Airplane

Estimation of the Spin and Recovery Characteristics of the North American XSN2J-1 Airplane

Free-Spinning and Tumbling Tests of a 1/16-Scale Model of the McDonnell XP-85 Airplane

Free-Spinning-Tunnel Tests of a 1/16-Scale Model of the Chance Vought XF5U-1 Airplane, TED No. NACA 2349

Free-Spinning-Tunnel Tests of a 1/35-Scale Model of the Douglas XB-43 Airplane

Measurements of Atmospheric Turbulence on Seattle-Alaska Airways

Comparison of Wind-Tunnel Predictions with Flight Measurements of the Longitudinal-Stability and -Control Characteristics of a Douglas BTD-1 Airplane

Compilation of Test Data on 111 Free-Spinning Airplane Models Tested in the Langley 15-Foot and 20-Foot Free-Spinning Tunnels

Computed Temperature Distribution and Cooling of Solid Gas-Turbine Blades

Cooling of Gas Turbines 6 - Computed Temperature Distribution Through Cross Section of Water-Cooled Turbine Blade

Cyclic Engine Test of Cast Vitallium Turbine Buckets - I

Calculation of the Pressure Distribution on Bodies of Revolution in the Subsonic Flow of a Gas Part 1 - Axially Symmetrical Flow

Calculation of Wing Bending Moments and Tail Loads Resulting from the Jettison of Wing Tips During a Symmetrical Pull-Up

Cooling of Gas Turbines 1 - Effects of Addition of Fins to Blade Tips and Rotor, Admission of Cooling Air Through Part of Nozzles, and Change in Thermal Conductivity of Turbine Components

The Crystal Structure at Room Temperature of Six Cast Heat-Resisting Alloys

Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8, and 19XB-1 Jet-Propulsion Engines 2 - Analysis of Turbine Performance of the 19B-8 Engine

Tuft Studies of the Flow over a Wing at Four Angles of Sweep

Wind Tunnel Development of Means to Alleviate Buffeting of the North American XP-82 Airplane at High Speeds

Data Obtained in the Flight Measurements to Determine the Stability and Control Characteristics of a C-54D Airplane (AAF No. 42-72713) and a Summary of the Test Program

Wind-Tunnel Investigation of a 1/5-Scale Model of the Ryan XF2R Airplane

An Analysis of the Full-Floating Journal Bearing

Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8 and 19XB-1 Jet- Propulsion Engines: 4 - Analysis of Compressor Performance

Investigation of High-Performance Fuels in Multicylinder and in Single-Cylinder Engines at High and Cruising Engine Speeds

Investigation of Axial-Flow Fan and Compressor Rotors Designed for Three-Dimensional Flow

Investigation of Sea-Level Performance of I-16 Turbojet Engine at Zero Ram with XFR-1 Intake Duct Shroud, and Tail Pipe

Longitudinal Stability and Stalling Characteristics of a 1/8.33-Scale Model of the Republic XF-12 Airplane

A Low-Speed Investigation of a Fuselage-Side Air Inlet for use at Transonic Flight Speeds

Knock-Limited Power Outputs from a CFR Engine Using Internal Coolants 3 - Four Alkyl Amines, Three Alkanolamines, Six Amides, and Eight Heterocyclic Compounds

Langley Full-Scale-Tunnel Investigation of Maximum Lift and Stability Characteristics of an Airplane Having Approximately Triangular Plan Form (DM-1 Glider)

On the Problems of Chaplygin for Mixed Sub-and Supersonic Flows

Pressure Distribution Measurements on a Turbine Rotor Blade Passing Behind a Turbine Nozzle Lattice

Rockets Using Liquid Oxygen

Rocket Power Plants Based on Nitric Acid and their Specific Propulsive Weights

Report on Rocket Power Plants Based on T-Substance

The Monoplane as a Lifting Vortex Surface

The Oscillating Circular Airfoil on the Basis of Potential Theory

The Turbulent Flow in Diffusers of Small Divergence Angle

Wind-Tunnel Investigations on a Changed Mustang Profile with Nose Flap Force and Pressure-Distribution Measurements

Theory of Wings in Nonstationary Flow

Three-Component Force and Mass-Flow Measurement on a Jet Nacelle

Tunnel Correction for Compressible Subsonic Flow

Test Report on Three-and Six-Component Measurements on a Series of Tapered Wings of Small Aspect Ratio (Partial Report: Elliptic Wing)

Abstracts Pertaining to Seaplanes


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