TRAIL - Technical Report Archive and Image Library

Free-jet altitude investigation of a 20-inch ram-jet combustor with a rich inner zone of combustion for improved low-temperature-ratio operation

Effect of liner air-entry holes, fuel state, and combustor size on performance of an annular turbojet combustor at low pressures and high air-flow rates

Effect of fuel injectors and liner design on performance of an annular turbojet combustor with vapor fuel

Performance of an annular turbojet combustor having reduced pressure losses and using propane fuel

An engineering method for the determination of aeroelastic effects upon the rolling effectiveness of ailerons on swept wings

Small-scale transonic investigation of a 45 degree sweptback wing of aspect ratio 4 with combinations of nose-flap deflections and wing twist

The effect of initial rate of subsonic diffusion on the stable subcritical mass-flow range of a conical shock diffuser

An experimental study of five annular air inlet configurations at subsonic and transonic speeds

Investigations toward simplification of missile control systems

A study of the use of various high-lift devices on the horizontal tail of a canard airplane model as a means of increasing the allowable center-of-gravity travel

Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings

Impingement of Cloud Droplets on Aerodynamic Bodies as Affected by Compressibility of Air Flow Around the Body

Procedure for Measuring Liquid-Water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method

De-Icing and Runback Characteristics of Three Cyclic Electric, External De-Icing Boots Employing Chordwise Shedding

Impingement of Water Droplets on a Cylinder in an Incompressible Flow Field and Evaluation of Rotating Multicylinder Method for Measurement of Droplet-Size Distribution, Volume-Median Droplet-Size, and Liquid-Water Content in Clouds

Experimental Investigation of Radome Icing and Icing Protection

Experimental Investigation of Laminar-Boundary-Layer Control on an Airfoil Section Equipped With Suction Slots Located at Discontinuities in the Surface Pressure Distribution

Effect of Type of Porous Surface and Suction Velocity Distribution on the Characteristics of a 10.5 Percent-Thick Airfoil With Area Suction

A Small Pirani Gage for Measurements of Nonsteady Low Pressures

Theoretical Investigation of the Supersonic Lift and Drag of Thin, Sweptback Wings With Increased Sweep Near the Root

A Low-Speed Experimental Study of the Directional Characteristics of a Sharp-Nosed Fuselage Through a Large Angle-of-Attack Range at Zero Angle of Sideslip

The Drag of Finite-Length Cylinders Determined From Flight Tests at High Reynolds Numbers for a Mach Number Range From 0.5 to 1.3

Estimation of Hydrodynamic Impact Loads and Pressure Distributions on Bodies Approximating Elliptical Cylinders With Special Reference to Water Landings of Helicopters

Bearing Strengths of Some 75S-T6 and 14S-T6 Aluminum-Alloy Hand Forgings

Calculation and Measurement of Normal Modes of Vibration of an Aluminum-Alloy Box Beam With and Without Large Discontinuities

Application of Silver Chloride in Investigations of Elasto-Plastic States of Stress

Column Strength of H-Sections and Square Tubes in Postbuckling Range of Component Plates

An Investigation of the Experimental Aerodynamic Loading on a Model Helicopter Rotor Blade

Effects of Parallel-Jet Mixing on Downstream Mach Number and Stagnation Pressure With Application to Engine Testing in Supersonic Tunnels

Investigation of the Statistical Nature of the Fatigue of Metals

The Creep of Single Crystals of Aluminum

Subsonic Flow of Air Through a Single-Stage and a Seven-Stage Compressor

Influence of Rotor-Engine Torsional Oscillation on Control of Gas-Turbine Engine Geared to Helicopter Rotor

A Method for Calculating the Subsonic Steady-State Loading on an Airplane With a Wing of Arbitrary Plan Form and Stiffness

A Study of the Stability of the Incompressible Laminar Boundary Layer on Infinite Wedges

A Study of the Application of Power-Spectral Methods of Generalized Harmonic Analysis to Gust Loads on Airplanes

The Structure of Turbulence in Fully Developed Pipe Flow

A Digital Automatic Multiple Pressure Recorder

Reflection of a Weak Shock Wave From a Boundary Layer Along a Flat Plate 1: Interaction of Weak Shock Waves With Laminar and Turbulent Boundary Layers Analyzed by Momentum-Integral Method

Reflection of Weak Shock Wave From a Boundary Layer Along a Flat Plate 2: Interaction of Oblique Shock Wave With a Laminar Boundary Layer Analyzed by Differential-Equation Method

The Galvanic Corrosion Theory for Adherence of Porcelain-Enamel Ground Coats to Steel

Relation Between Roughness of Interface and Adherence of Porcelain Enamel to Steel

Appraisal of Hazards to Human Survival in Airplane Crash Fires

Supersonic Flow Past Oscillating Airfoils Including Nonlinear Thickness Effects

Estimation of Forces and Moments Due to Rolling for Several Slender-Tail Configurations at Supersonic Speeds

A Rapid Method for Use in Design of Turbines Within Specified Aerodynamic Limits

Flow Properties of Strong Shock Waves in Xenon Gas as Determined for Thermal Equilibrium Conditions

Counting Methods and Equipment for Mean-Value Measurements in Turbulence Research

Deflection of Delta Wings Having a Carry-Through-Bay Chord Smaller than the Wing Root Chord

The Effects of Camber on the Variation with Mach Number of the Aerodynamic Characteristics of a 10-Percent-Thick Modified NACA Four-Digit-Series Airfoil Section

Keyword Search

Published Year

Subject

Author