Browse TRAIL Inventories

A Thermodynamic Study of the Turbojet Engine

Approximate Formulas for the Computation of Turbulent Boundary-Layer Momentum Thicknesses in Compressible Flows

Charts for Critical Combinations of Longitudinal and Transverse Direct Stress for Flat Rectangular Plates

Knock-Limited Performance of N-Methylaniline and Xylidine Blends in an Air-Cooled Aircraft Cylinder

Determination of the Stability and Control Characteristics of a Straight-Wing, Tailless Fighter-Airplane Model in the Langley Free-Flight Tunnel

Comparison of Tail and Wing-Tip Spin-Recovery Parachutes as Determined by Tests in the Langley 20-Foot Free-Spinning Tunnel

The Effect of Lateral Area on the Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Langley Free-Flight Tunnel

The Lagrangian Multiplier Method of Finding Upper and Lower Limits to Critical Stresses of Clamped Plates

Determination of Gas Temperatures from the Frequency of Knock-Induced Gas Vibrations in an Internal-Combustion Engine

Summary of Drag Characteristics of Practical-Construction Wing Sections

Cylinder-Temperature Correlation of a Single-Cylinder Liquid-Cooled Engine

Distribution of Structural Weight of Wing Along the Span

Effect of Compressibility on the Pressure and Forces Acting on a Modified NACA 65,3-019 Airfoil Having a 0.20-Chord Flap

Two-Dimensional Irrotational Mixed Subsonic and Supersonic Flow of a Compressible Fluid and the Upper Critical Mach Number

A Study of Combustion in a Flowing Gas

Application of the Method of Characteristics to Supersonic Rotational Flow

Lightning Discharges to Aircraft and Associated Meteorological Conditions

Effects of Specific Types of Surface Roughness on Boundary-Layer Transition

An Empirical Equation for the Coefficient of Heat Transfer to a Flat Surface From a Plane Heated-Air Jet Directed Tangentially to the Surface

Stress Analysis of Columns and Beam Columns by the Photoelastic Method

The Column Strength of Aluminum Alloy 75S-T Extruded Shapes

A Simplified Method for Determining From Flight Data the Rate of Change of Yawing-Moment Coefficient With Sideslip

Note on the Theorems of Bjerknes and Crocco

Standard Nomenclature for Airspeeds With Tables and Charts for Use in Calculation of Airspeed

The Synthesis and Purification of Aromatic Hydrocarbons 4: 1,2,3-Trimethylbenzene

The Synthesis and Purification of Aromatic Hydrocarbons 1: Butylbenzene

Standard Procedures for Rating and Testing Multistage Axial-Flow Compressors

Methods for Determination and Computation of Flow Patterns of a Compressible Fluid

Application of the Method of Characteristics to Supersonic Rotational Flow

The Crystal Structure at Room Temperature of Eight Forged Heat-Resisting Alloys

A General Method of Selecting Foam Inhibitors

Experimental Determination of the Effects of Directional Stability and Rotary Damping in Yaw on Lateral Stability and Control Characteristics

Quantitative Treatment of the Creep of Metals by Dislocation and Rate-Process Theories

Pressure Distributions for Representative Airfoils and Related Profiles

Summary and Analysis of Data on Damping in Yaw and Pitch for a Numbers of Airplane Models

Consideration of Dynamic Loads on the Vertical Tail by the Theory of Flat Yawing Maneuvers

Turbosupercharger-Rotor Temperatures in Flight

A Condition on the Initial Shock

The Lagrangian Multiplier Method of Finding Upper and Lower Limits to Critical Stresses of Clamped Plates

Extension of the Chaplygin Proofs on the Existence of Compressible-Flow Solutions to the Supersonic Region

A Discussion of the Application of the Prandtl-Glauert Method to Subsonic Compressible Flow Over a Slender Body of Revolution

Stress Rupture of Heat Resisting Alloys as a Rate Process

Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow 1: Circulatory Flows Obeying the Simplified Density-Speed Relation

Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow 2: Subsonic Symmetric Adiabatic Flows

On Supersonic and Partially Supersonic Flows

Wind-Tunnel Investigation of the Effect of Canopies on Directional Stability Characteristics of a Single Engine Airplane Model

Lifting-Surface-Theory Results for Thin Elliptic Wings of Aspect Ratio 3 with Chordwise Loadings Corresponding to 0.5-Chord Plain Flap and to Parabolic-Arc Camber

Column Strength of Aluminum Alloy 14S-T Extruded Shapes and Rod

Stress-Strain and Elongation Graphs for Aluminum Alloy R301 Sheet

Effects of Axial-Plane Curvature and Passage-Area Variation on Flow Capacity of Radial-Discharge Impeller with Conventional Inlet Buckets


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