TRAIL - Technical Report Archive and Image Library

Limited Investigation of Effects of Differential Horizontal-Tail Deflection on Lateral Control Characteristics of Two Swept-Wing Airplane Models at Mach Numbers From 1.4 to 2.0

Data From Large-Scale Low-Speed Tests of Airplane Configurations With a Thin 45 Degree Swept-Wing Incorporating Several Leading-Edge Contour Modifications

Effect of Several Wing Modifications on the Subsonic and Transonic Longitudinal Handling Qualities of the Douglas D-558-II Research Airplane

Model Ditching Investigation of a Jet Transport Airplane With Various Engine Installations

Experimental Hinge Moments on Freely Oscillating Flap-Type Control Surfaces

Investigation of the Ni(sub 3)Al Phrase of Nickel-Aluminum Alloys

Experimental Investigation at Low Speed of the Effects of Wing Position on the Static Stability of Models Having Fuselages of Various Cross Section and Unswept and 45 Degrees Sweptback Surfaces

Correlation Between Hydrogen Pressure and Protective Action of Additives in the Molten Sodium Hydroxide - Nickel System

Effect of an Adjustable Supersonic Inlet on the Performance Up to Mach Number 2.0 of a J34 Turbojet Engine

Flutter Tests of a 1/25-Scale Model of the B-36J/RF-84F Tip-Coupled Airplane Configuration in the Langley 19-Foot Pressure Tunnel

Flight Investigation of the Performance of a Two-Stage Solid-Propellant Nike-Deacon (DAN) Meteorological Sounding Rocket

Supersonic Investigation of the Lift, Drag, Static Stability, and Hinge-Moment Characteristics of a Rocket-Powered Model of a Ballistic-Missile Configuration

Perforated Sheets as a Porous Material for Distributed Suction and Injection

The Subsonic Lateral and Longitudinal Static Stability Characteristics Up to Large Angles of Sideslip for a Triangular-Wing Airplane Model Having a Ventral Fin

Some Linear Dynamics of Two-Spool Turbojet Engines

Stall Propagation in Axial-Flow Compressors

Space Heating Rates for Some Premixed Turbulent Propane-Air Flames

Hydrodynamic Impact Loads in Smooth Water for a Prismatic Float Having an Angle of Dead Rise of 10 Degrees

Generalized Tables of Corrections to Thermodynamic Properties for Nonpolar Gases

Attenuation in a Shock Tube Due to Unsteady-Boundary-Layer Action

A Theory for the Elastic Deflections of Plates Integrally Stiffened on One Side

Tabulation of the F(Sub Lambda) Functions Which Occur in the Aerodynamic Theory of Oscillating Wings in Supersonic Flow

Influence of Temperature on Creep, Stress-Rupture and Static Properties of Melamine-Resin and Silicone-Resin Glass-Fabric Laminates

Influence of Large Amplitudes on Flexural Motions of Elastic Plates

Thermodynamic Properties of Gaseous Nitrogen

Time Correlator for Problems in Aerodynamics

Effect of Carriage Mass Upon the Loads and Motions of a Prismatic Body During Hydrodynamic Impact

Wind-Tunnel Investigation of a Number of Total-Pressure Tubes at High Angles of Attack: Subsonic, Transonic, and Supersonic Speeds

Mechanism of Generation of Pressure Waves at Flame Fronts

Investigation of Far Noise Field of Jets 1: Effect of Nozzle Shape

Vapor-Phase Oxidation and Spontaneous Ignition-Correlation and Effect of Variables

Correlation, Evaluation, and Extension of Linearized Theories for Tire Motion and Wheel Shimmy

Linearized Lifting-Surface and Lifting-Line Evaluations of Sidewash Behind Rolling Triangular Wings at Supersonic Speeds

Charts for Estimating Rotor-Blade Flapping Motion of High-Performance Helicopters

A Simplified Method for Approximating the Transient Motion in Angles of Attack and Sideslip During a Constant Rolling Maneuver

Measurement of Static Pressure on Aircraft

Remark on the Theory of Lifting Surfaces

On the Gas Dynamics of a Rotating Impeller

An analysis of buzzing in supersonic ram jets by a modified one-dimensional nonstationary wave theory

Analysis and comparison with theory of flow-field measurements near a lifting rotor in the Langley full-scale tunnel

Experimental investigation of air-cooled turbine rotor blade temperatures in a turbojet engine operating at turbine-inlet temperatures up to 2580 R and altitudes of 50,000 and 60,000 feet

Experimental investigation on the Langley helicopter test tower of compressibility effects on a rotor having NACA 63₂-015 airfoil sections

Method for Shortening Ram-Jet Engines by Burning Hydrogen Fuel in the Subsonic Diffuser

Flight Investigation of the Effect of a Propulsive Jet Positioned According to the Transonic Area Rule on the Drag Coefficients of a Single-Engine Delta-Wing Configuration at Mach Numbers From 0.83 to 1.36

A Flight Investigation of the Handling Characteristics of a Fighter Airplane Controlled Through a Rate Type of Automatic Control System

A Flight Investigation of the Handling Characteristics of a Fighter Airplane Controlled Through an Attitude Type of Automatic Pilot

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