Browse TRAIL Inventories

Tests of the NACA 0010-1.50 40/1.051 Airfoil Section at High Subsonic Mach Numbers

Cooperative Investigation of Relationship Between Static and Fatigue Properties of Wrought N-155 Alloy at Elevated Temperatures

Supersaturation in the Spontaneous Formation of Nuclei in Water Vapor

The Microstructure of Turbulent Flow

Plastic Deformation of Aluminum Single Crystals at Elevated Temperatures

Concerning the Flow About Ring-Shaped Cowlings 12: Two New Classes of Circular Cowls

Steady Vibrations of Wing of Circular Plan Form

Concerning the Flow on Ring-Shaped Cowlings Part 13: The Influence of a Projecting Hub

Calculation of the Shape of a Two-Dimensional Supersonic Nozzle in Closed Form

Deflection and Stress Analysis of Thin Solid Wings of Arbitrary Plan Form with Particular Reference to Delta Wings

One-Dimensional Analysis of Choked-Flow Turbines

Theoretical Prediction of Pressure Distributions on Nonlifting Airfoils at High Subsonic Speeds

Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems: Effect of Missile Configuration on the Speed of Response

A Method for Estimating the Rolling Moments Caused by Wing-Tail Interference for Missiles at Supersonic Speeds

Investigation of Pressure Recovery of a Single-Conical-Shock Nose Inlet at Mach Number 5.4

Weight Bar Charts

Criticality Survey of Hydroxides as Coolant Moderators for Aircraft Nuclear Reactors

Summary Report on Analytical Evaluation of Air and Fuel Specific-Impulse Characteristics of Several Nonhydrocarbon Jet-Engine Fuels

Static Longitudinal Stability and Control Characteristics of a 1/16 -Scale Model of the Douglas D-558-II Research Airplane at Mach Numbers of 1.61 and 2.01

Performance Characteristics of a Double-Cylindrical-Shroud Ejector Nozzle

Wind-Tunnel Investigation of the Motion of a 1/10-Scale Model of the Douglas XF4D-1 Escape Capsule When Jettisoned by Jet Ejection: TED No. NACA DE 359

The Low-Speed Lift and Drag Characteristics of a Series of Airplane Models Having Triangular or Modified Triangular Wings

Damping in Pitch of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds

Effect of Large Deflection of a Canard Control and Deflections of a Wing-Tip Control on the Static-Stability and Induced-Roll Characteristics of a Cruciform Canard Missile at a Mach Number of 2.01

Effects of External Store Mounting on the Buffet, Trim, and Drag Characteristics of Rocket-Powered Fuselage and Store Combinations Between Mach Numbers of 0.7 and 1.4

Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine 13: Endurance Evaluation of Several Protective Coatings Applied to Turbine Blades of Nonstrategic Steels

Effects of Span and Spanwise and Chordwise Location on the Control Effectiveness of Spoilers on a 50 Degree Sweptback Wing at Mach Numbers of 1.41 and 1.96

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


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