Browse TRAIL Inventories

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

Acceleration Measurements During Landing in Rough Water of a 1/7-Scale Dynamic Model of Grumman XJR2F-1 Amphibian - Langley Tank Model 212: TED No. NACA 2378

Aerodynamic Characteristics at High Speeds of Full-Scale Propellers Having Different Shank Designs

The Flow Through Axial Turbine Stages of Large Radial Blade Length

Fundamentals of the Control of Gas-Turbine Power Plants for Aircraft, Part 3: Control of Jet Engines

Fundamental Aerodynamic Investigations for Development of Arrow-Stabilized Projectiles

Fundamentals of the Control of Gas-Turbine Power Plants for Aircraft, Part 2: Principles of Control Common to Jet, Turbine-Propeller Jet, and Ducted-Fan Jet Power Plants

Fundamentals of the Control of Gas-Turbine Power Plants for Aircraft, Part 1: Standardization of the Computations Relating to the Control of Gas-Turbine Power Plants for Aircraft by the Employment of the Laws of Similarity

The Lift Distribution of Swept-Back Wings

Laboratory Report on the Investigation of the Flow Around Two Turbine-Blade Profiles Using the Interferometer Method

Lift Increase by Blowing Out Air, Tests on Airfoil of 12 Percent Thickness, Using Various Types of Flap

Effects of Induction-System Icing on Aircraft-Engine Operating Characteristics

Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms July 12, 1947 to July 18, 1947 at Clinton County Army Air Field, Ohio

Evaluation of Gust and Draft Velocities from Flights of P-61C Airplanes within Thunderstorms July 24, 1946 to August 6, 1946 at Orlando, Florida

Investigation of Single-Stage Modified Turbine of Mark 25 Torpedo Power Plant

An Investigation of the Aerodynamic Characteristics of an 0.08-Scale Model of the Chance Vought XF7U-1 Airplane in the Langley High-Speed 7- by 10-Foot Tunnel Part 5 - Wing-Alone Tests and Effect of Modifications to the Vertical Fins, Speed Brakes, and Fuselage TED No. NACA DE308, Part V, Wing-Alone Tests and Effect of Modifications to the Vertical Fins, Speed Brakes, and Fuselage, TED No. NACA DE308

Flight Measurements of the Flying Qualities of a Lockheed P-80A Airplane (Army No. 44-85099) - Stalling Characteristics

Free-Spinning Tunnel Tests of a 1/24-Scale Model of the Grumman XTB3F-1 Airplane, TED No. NACA DE304

Aerodynamic Characteristics of a Portion of the Horizontal Tail from a Douglas C-74 Airplane with Fabric-Covered Elevators

Aerodynamic Characteristics of Three Deep-Stepped Planing-Tail Flying-Boat Hulls

Ditching Tests with a 1/16-Size Model of the Navy XP2V-1 Airplane at the Langley Tank No. 2 Monorail

Spin and Recovery Characteristics of the Curtiss-Wright XP-87 Airplane

Supplementary Free-Spinning-Tunnel Tests of a 1/16-Scale Model of the McDonnell XB-85 Airplane Equipped with a Conventional-Tail Arrangement

Supplementary Data on Airspeeds and Mach Numbers Attained by Lockheed Constellation Airplanes in Transcontinental Operations

Supersonic Wave Drag of Sweptback Tapered Wings at Zero Lift

Tests of Submerged Duct Installation on the Ryan FR-1 Airplane in the Ames 40- by 80-Foot Wind Tunnel


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