Browse TRAIL Inventories

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

Moments of Cambered Round Bodies

Investigations Relating to the Extension of Laminar Flow by Means of Boundary-Layer Suction Through Slots

Observations of Icing Conditions Encountered in Flight During 1948

Remarks Concerning the Behavior of the Laminar Boundary Layer in Compressible Flows

Shear Buckling of Infinitely Long Simply Supported Metalite Type Sandwich Plates

Provisional Symbols and Definitions for Aircraft Turbines

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

The Buckling of Parallel Simply Supported Tension and Compression Members Connected by Elastic Deflectional Springs

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


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