Browse TRAIL Inventories

Grain-Boundary Behavior in Creep of Aluminum Bicrystals

Ground-Simulator Study of the Effects of Stick Force and Displacement on Tracking Performance

Measurements of Turbulent Skin Friction on a Flat Plate at Transonic Speeds

Second Order Subsonic Airfoil-Section Theory and Its Practical Application

Investigation of Jet-Engine Noise Reduction by Screens Located Transversely Across the Jet

Effect of Oxygen Content of Furnace Atmosphere on Adherence of Vitreous Coatings to Iron

Tables of Coefficients for the Analysis of Stresses About Cutouts in Circular Semimonocoque Cylinders with Flexible Rings

Total Lift and Pitching Moment on Thin Arrowhead Wings Oscillating in Supersonic Potential Flow

Contributions on the Mechanics of Boundary-Layer Transition

Flight Investigation of the Surface-Pressure Distribution and the Flow Field Around a Conical and Two Spherical Nonrotating Full-Scale Propeller Spinners

Influence of Shear Deformation of the Cross Section on Torsional Frequencies of Box Beams

Supplementary Charts for Estimating Performance of High-Performance Helicopters

Charts for Estimating Performance of High-Performance Helicopters

Theoretical Investigation of a Proportional-Plus-Flicker Automatic Pilot

A Study of Normal Accelerations and Operating Conditions Experienced by Helicopters in Commercial and Military Operations

An Approximate Solution for Axially Symmetric Flow Over a Cone With an Attached Shock Wave

Some Measurements of Time and Space Correlation in Wind Tunnel

The Theories of Turbulence

Interaction of a Free Flame Front With a Turbulence Field

Nonlifting Wing-Body Combinations With Certain Geometric Restraints Having Minimum Wave Drag at Low Supersonic Speeds

On the Mechanism of Buckling of a Circular Cylindrical Shell Under Axial Compression

Optimum Flight Paths of Turbojet Aircraft

Steady Properly-Banked Turns of Turbojet-Propelled Airplanes

A Method of Quadrature for Calculation of the Laminar and Turbulent Boundary Layer in Case of Plane and Rotationally Symmetrical Flow

General Solutions of Optimum Problems in Nonstationary Flight

Incompressible Flutter Characteristics of Representative Aircraft Wings

Effect of Interaction on Landing-Gear Behavior and Dynamic Loads in a Flexible Airplane Structure

Theory of Dynamic Creep

Theory of Reversible and Nonreversible Cracks in Solids

Influence of Alloying upon Grain-Boundary Creep

Metallography of Aluminum and Its Alloys: Use of Electrolytic Polishing

Influence of Hot-Working Conditions on High-Temperature Properties of a Heat-Resistant Alloy

Linearized Lifting-Surface and Lifting-Line Evaluations of Sidewash Behind Rolling Triangular Wings at Supersonic Speeds

Contributions on the Mechanics of Boundary-Layer Transition

Charts for Estimating Performance of High-Performance Helicopters

Characteristics of Turbulence in Boundary Layer with Zero Pressure Gradient

Some Results of Flight Testing of Ski-Equipped Aircraft at the Naval Air Test Center

Investigation of a Cermet Gas-Turbine-Blade Material of Titanium Carbide Infiltrated With Hastalloy C

Study of Effects of Microstructure and Anisotropy on Fatigue of 23S-T4 Aluminum Alloy

Application of Stream-Filament Techniques to Design of Diffuser Between Compressor and Combustor in a Gas-Turbine Engine

Flight Measurements of the Dynamic Lateral and Longitudinal Stability of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback

The Effect of a 4-Percent-High Spoiler on Buffeting Forces on a NACA 65(Sub 06)A004 Two-Dimensional Airfoil at Subsonic Mach Numbers

Effects of Wing Position and Fuselage Size on the Low-Speed Static Rolling Stability Characteristics of a Delta-Wing Model

Hydrodynamic Pressure Distribution Obtained With a Streamline Body Equipped With Chine Strips

Free-Flight Tests to Determine the Power-on and Power-Off Pressure Distribution and Drag of the NACA RM-10 Research Vehicle at Large Reynolds Numbers Between Mach Numbers 0.8 and 3.0

Theoretical Calculations of the Pressures, Forces, and Moments Due to Various Lateral Motions Acting on Thin Isolated Vertical Tails With Supersonic Leading and Trailing Edges

Investigation of the Effects of an Airfoil Section Modification on the Aerodynamic Characteristics at Subsonic and Supersonic Speeds of a Thin Swept Wing of Aspect Ratio 3 in Combination With a Body

Thermal Analysis of Sodium Hydroxide Containing the Reaction Products of Sodium Hydroxide and Chromium Metal

Preliminary Investigation of Several Root Designs for Cermet Turbine Blades in Turbojet Engine 3: Curved-Root Design

Meteorological Problems Associated With Commercial Turbojet-Aircraft Operation


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