Browse TRAIL Inventories

The Response of Pressure Measuring Systems to Oscillating Pressures

Notes on the Foundations of the Theory of Small Displacements of Orthotropic Shells

Effect of Automatic Stabilization on the Lateral Oscillatory Stability of a Hypothetical Airplane at Supersonic Speeds

Hydrodynamic Impact Loads in Smooth Water for a Prismatic Float Having an Angle of Dead Rise of 40 Degrees

Critical Combinations of Shear and Direct Axial Stress for Curved Rectangular Panels

Wind-Tunnel Investigation of an NACA 65-210 Semispan Wing Equipped With Circular Plug Ailerons and a Full-Span Slotted Flap

Theory of the Inlet and Exhaust Processes of Internal-Combustion Engines

Summary of Information Relating to Gust Loads on Airplanes

A Rapid Graphical Method for Computing the Pressure Distribution at Supersonic Speeds on a Slender Arbitrary Body of Revolution

On Compressibility Corrections for Subsonic Flow Over Bodies of Revolution

Observations on the Maximum Average Stress of Flat Plates Buckled in Edge Compression

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


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