Browse TRAIL Inventories

Investigation of the Effects of Leading-Edge Chord-Extensions and Fences in Combination with Leading-Edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4

Determination of the Elastic Constants of Airplane Tires

Slowing-Down Distribution to Indium Resonance of Neutrons From a Ra-Alpha-Be Source in Water-Iron Mixtures

Theoretical Maximum Performance of Liquid Fluorine - Liquid Oxygen Mixtures With JP-4 Fuel as Rocket Propellants

Pumping Characteristics for Several Simulated Variable-Geometry Ejectors With Hot and Cold Primary Flow

On the Use of the Indicial-Function Concept in the Analysis of Unsteady Motions of Wings and Wing-Tail Combinations

Flame Quenching by a Variable-Width Rectangular-Slot Burner as a Function of Pressure for Various Propane-Oxygen-Nitrogen Mixtures

Wind-Tunnel Investigation at a Mach Number of 2.01 of the Aerodynamic Characteristics in Combined Pitch and Sideslip of Some Canard-Type Missiles Having Cruciform Wings and Canard Surfaces With 70 Degree Delta Plan Forms

Study of Some Dielectric Properties of Suspensions of Magnesium Particles in Mineral Oil

A Survey of Background and Aircraft Noise in Communities Near Airports

Low-Speed Measurements of Rolling and Yawing Stability Derivatives of a 60 Degree Delta-Wing Model

The Effects of Horizontal-Tail Height and a Partial-Span Leading-Edge Extension on the Static Longitudinal Stability of a Wing-Fuselage-Tail Combination Having a Sweptback Wing

The Effects of Circular End Plates on the Lift, Drag, and Pitching Moment at Subsonic and Supersonic Speeds on a Modified Triangular Wing Having an Aspect Ratio of 2, a Taper Ratio of 0.33, and a 45 Degree Swept Leading Edge

Effects of Some Metal Additions on Properties of Molybdenum Disilicide

An Experimental Investigation of Two-Dimensional, Supersonic Cascade-Type Inlets at a Mach Number of 3.11

Experimental Evidence of Sustained Coupled Longitudinal and Lateral Oscillations From a Rocket-Propelled Model of a 35 Degree Swept Wing Airplane Configuration

High-Temperature Lubricants and Bearings for Aircraft Turbine Engine

Rapid Estimation of Bending Frequencies of Rotating Beams

Summary of 65-Series Compressor-Blade Low-Speed Cascade Data by Use of the Carpet-Plotting Technique

Preliminary Investigation of Stress-Rupture and Tensile Strength of Thermenol, an Iron-Aluminum Alloy

Preliminary Measurements of Turbulence and Temperature Fluctuations Behind a Heated Grid

Speed-Brake Investigation at Low Speed of a 1/10-Scale Model of the MX-1554A Airplane With a Circular Jet Nozzle

Compatibility of Pentaborane With Materials Used for Seals, Gaskets, and Construction

Review of High-Performance Axial-Flow-Compressor Blade-Element Theory

An Analysis of Pressure Studies and Experimental and Theoretical Downwash and Sidewash Behind Five Pointed-Tip Wings at Supersonic Speeds

Comparison Between Theoretical and Experimental Rates of Roll of Two Models with Flexible Rectangular Wings at Supersonic Speeds

Investigation of Conical Subsonic Diffusers for Ram-Jet Engines

Experimental Investigation at High Subsonic Speeds to Determine the Rolling-Stability Derivatives of Three Wing-Fuselage Configurations

Pressure, Recovery and Mass-Flow Performance of Four Annular Nose Inlets Operating in Mach Number Region of 3.1 and Reynolds Number Range of Approximately 0.45 x 10(exp 6) to 2.20 x 10(exp 6)

The Effect of a Change in Body Shape on the Loading of a 45 Degree Sweptback Wing-Body Combination at Transonic Speeds

Static Longitudinal Stability Characteristics of a Composite-Plan-Form-Wing-Model Including Some Comparisons with a 45 Degree Sweptback Wing at Transonic Speeds

Lateral Motions Encountered with the Douglas D-558-II All-Rocket Research Airplane During Exploratory Flights to a Mach Number of 2.0

Quasi-Cylindrical Theory of Wing-Body Interference at Supersonic Speeds and Comparison with Experiment

Application of Pulse Techniques to Strain Gages

Investigation of Turbojet Engine Performance at Speeds and Gas Temperatures Above Rated Using Turbine-Blade External Water-Spray Cooling from Stationary Injection Orifices

Longitudinal Stability Characteristics in Accelerated Maneuvers at Subsonic and Transonic Speeds of the Douglas D-558-II Research Airplane Equipped with a Leading-Edge Wing Chord-Extension

Experimental Investigation of a Five-Stage Axial-Flow Research Compressor with Transonic Rotors in All Stages 1: Compressor Design

Experimental Investigation of a Five-Stage Axial-Flow Research Compressor With Transonic Rotors in All Stages 2: Compressor Over-All Performance

Investigation of a Flow Deflector and an Auxiliary Scoop for Improving Off-Design Performance of Nose Inlets

An Investigation of the Effects of Jet Exhaust and Reynolds Number Upon the Flow Over the Vertical Stabilizer and Rudder of the Douglas D-558-II Research Airplane at Mach Numbers of 1.62, 1.93, and 2.41

Effects of Operating Propellers on the Wing-Surface Pressures of a Four-Engine Tractor Airplane Configuration Having a Wing with 40 Degrees of Sweepback

Effects of Resin Coating Methods and Other Variables on Physical Properties of Glass-Fabric Reinforced Polyesters

Two-Spool Matching Procedures and Equilibrium Characteristics of a Two-Spool Turbojet Engine

Effect at Transonic Speeds of Inboard Spoilers on the Static Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing-Body Combination Having a Leading-Edge Chord-Extension

Organophosphorus Compounds in Rocket-Engine Applications

Preliminary Flight Measurements of the Total-Pressure Recovery of a Split-Wing Ram-Jet Inlet at Mach Numbers from 1.4 to 3.16

Experimental Investigation of Sublimation of Ice at Subsonic and Supersonic Speeds and Its Relation to Heat Transfer

Speed-Brake Investigation at Low Speed of a 1/10-Scale Model of the MX-1554A Airplane With a Circular Jet Nozzle

Preliminary Performance Data Obtained in a Full-Scale Free-Jet Investigation of a Side-Inlet Supersonic Diffuser

On the Three-Dimensional Instability of Laminar Boundary Layers on Concave Walls


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