Browse TRAIL Inventories

Effect of Thickness on the Lateral Force and Yawing Moment of a Sideslipping Delta Wing at Supersonic Speeds

Thermodynamic Charts for Internal-Combustion-Engine Fluids

Elastic Buckling of a Simply Supported Plate Under a Compressive Stress That Varies Linearly in the Direction of Loading

Elastic Buckling of Outstanding Flanges Clamped at One Edge and Reinforced by Bulbs at Other Edge

On Internal Damping of Rotating Beams

NACA and Office of Naval Research Metallurgical Investigation of Two Large Forged Discs of S-590 Alloy

Office of Naval Research and NACA Metallurgical Investigation of a Large Forged Disc of Inconel X Alloy

Office of Naval Research and NACA Metallurgical Investigation of a Large Forged Disc of S-816 Alloy

Experimental Investigation of Moving Pressure Disturbances and Shock Waves and Correlation with One-Dimensional Unsteady-Flow Theory

Flight Investigation in Climb and at High Speed of a Two-Blade and a Three-Blade Propeller

Matrix Methods for Calculating Cantilever-Beam Deflections

A Comparison of Wing Loads Measured in Flight on a Fighter-Type Airplane by Strain-Gage and Pressure Distribution Methods

Reinforced Circular Cutouts in Plane Sheets

Quantitative Study of Variations in Concentration of Glycerol and Aerosol OT on Foaming Volume of Oil at Room Temperature

Direct-Reading Design Charts for 24S-T Aluminum-Alloy Flat Compression Panels Having Longitudinal Formed Z-Section Stiffeners

Summary of the Availability and Performance Problems of High Octane Number Fuels

Preliminary Investigation of 3-Inch Slotted Transonic Wind-Tunnel Test Sections

Spin-Tunnel Investigation of the Jettisoning of External Fuel Tanks in Spins

Bibliography of Classified Aircraft-Fire Literature

Study by NACA Wing-Flow Method of Transonic Drag Characteristics of a Blunt-Nose Body of Revolution and Comparison with Results for a Sharp-Nose Body

Pressure Distributions on Thin Conical Body of Elliptic Cross Section at Mach Number 1.89

Preliminary Aerodynamic Investigation of the Effect of Camber on a 60 Degree Delta Wing with Round and Beveled Leading Edges

Investigation of Performance of Typical Inlet Stage of Multistage Axial-Flow Compressor

Lateral-Control Investigation on a 37 Degree Sweptback Wing of Aspect Ratio 6 at a Reynolds Number of 6,800,000

An Empirical Method for Estimating Trailing-Edge Loads at Transonic Speeds

The Static-Pressure Error of Wing and Fuselage Airspeed Installations of the X-1 Airplanes in Transonic Flight

Tests of the NACA 64-010 and 64A010 Airfoil Sections at High Subsonic Mach Numbers

Investigation of Fretting by Microscopic Observation

Effect of Reynolds Number in Turbulent-Flow Range on Flame Speeds of Bunsen Burner Flames

Application of Radial-Equilibrium Condition to Axial-Flow Compressor and Turbine Design

Line-Vortex Theory for Calculation of Supersonic Downwash

Correlation of Physical Properties With Molecular Structure for Some Dicyclic Hydrocarbons Having High Thermal-Energy Release Per Unit Volume

Equilibrium Operating Performance of Axial-Flow Turbojet Engines by Means of Idealized Analysis

Plastic Buckling of a Rectangular Plate Under Edge Thrusts

On Stability of Free Laminar Boundary Layer Between Parallel Streams

Investigation of Separation of the Turbulent Boundary Layer

Characteristics of Low-Aspect-Ratio Wings at Supercritical Mach Numbers

Calculation of Counterrotating Propellers

Behavior of the Laminar Boundary Layer for Periodically Oscillating Pressure Variation

The Characteristics Method Applied to Stationary Two-Dimensional and Rotationally Symmetrical Gas Flows

A Class of de Laval Nozzles

Compression Shocks in Two-Dimensional Gas Flows

The Effect of Air Jets Simulating Chines or Multiple Steps on the Hydrodynamic Characteristics of a Streamline Fuselage

Summary of Information Relating to Gust Loads on Airplanes

Stability Results Obtained With Douglas D-558-1 Airplane (BuAero No. 37971) in Flight Up to a Mach Number of 0.89

Stability and Control Data Obtained from First Flight of X-4 Airplane

Langley Free-Flight-Tunnel Investigation of the Automatic Lateral Stability Characteristics of a Model Equipped with a Gyro Stabilizing Unit that Provided either Flicker-Type or Hunting Control

On Reflection of Shock Waves from Boundary Layers

Investigation of Aerodynamic and Icing Characteristics of Recessed Fuel-Vent Configurations

Investigation of Icing Characteristics of Typical Light Airplane Engine Induction Systems


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