Browse TRAIL Inventories

An evaluation of air-borne radar as a means of avoiding atmospheric turbulence

A study of skin temperatures of conical bodies in supersonic flight

Tests of a triangular wing of aspect ratio 2 in the Ames 12-foot pressure wind tunnel. 1: the effect of Reynolds number and Mach number on the aerodynamic characteristics of the wing with flap undeflected

Additional Abstracts Pertaining to Seaplanes

AVA monographs. B: Boundary layer

Effects of Ice Formations on Airplane Performance in Level Cruising Flight

NACA: University Conference on Aerodynamics: A Compilation of the Papers Presented

Hydrodynamic Characteristics of a Low-Drag, Planing-Tail Flying-Boat Hull

Icing and De-Icing of a Propeller with Internal Electric Blade Heaters

Determination of Stresses in Gas-turbine Disks Subjected to Plastic Flow and Creep

De-Icing Effectiveness of External Electric Heaters for Propeller Blades

Plate Compressive Strength of FS-1H Magnesium-Alloy Sheet and a Maximum-Strength Formula for Magnesium-Alloy and Aluminum-Alloy Formed Sections

Experimental Investigation of the Jet-Boundary Constriction Correction for a Model Spanning a Closed Circular Tunnel

Experimental Study of Effect of Vaneless-Diffuser Diameter on Diffuser Performance

Temperature Gradients in the Wing of a High-Speed Airplane During Dives From High Altitudes

Spray Characteristics of Four Flying-Boat Hulls as Affected by Length-Beam Ratio

Supersonic Nozzle Design

X-Ray Diffraction Investigation of Minor Phases of 20 High-Temperature Alloys

Thermodynamic Charts for the Computation of Fuel Quantity Required for Constant-Pressure Combustion With Diluents

Shear Lag in a Plywood Sheet-Stringer Combination Used for the Chord Member of a Box Beam

Effect of Local Boiling and Air Entrainment on Temperatures of Liquid-Cooled Cylinders

Effect of Preignition on Cylinder Temperatures, Pressures, Power Output, and Piston Failures

Effect of Shear Lag on Bending Vibration of Box Beams

Effect of Strength and Ductility on Burst Characteristics of Rotating Disks

Determination of Coupled and Uncoupled Modes and Frequencies of Natural Vibration of Swept and Unswept Wings From Uniform Cantilever Modes

Charts for the Computation of Equilibrium Composition of Chemical Reactions in the Carbon-Hydrogen-Oxygen-Nitrogen System at Temperatures From 2000 to 5000 K

Calculation of Uncoupled Modes and Frequencies in Bending or Torsion of Nonuniform Beams

Charts for the Analysis of One-Dimensional Steady Compressible Flow

Calibration of Altimeters Under Pressure Conditions Simulating Dives and Climbs

Measurements of the Pressure Distribution on the Horizontal-Tail Surface of a Typical Propeller-Driven Pursuit Airplane in Flight 3: Tail Loads in Abrupt Pull-Up Push-Down Maneuvers

An Investigation of Aircraft Heaters 29: Comparison of Several Methods of Calculating Heat Losses From Airfoils

An Investigation of Aircraft Heaters 27: Distribution of Heat-Transfer Rate in the Entrance Section of a Circular Tube

Investigation of Axial-Flow Fan and Compressor Rotors Designed for Three-Dimensional Flow

Flight Measurements of Buffeting Tail Loads

Knock-Limited Performance of Several Branched Paraffins and Olefins

Analysis of Flight-Performance Measurements on a Twisted, Plywood-Covered Helicopter Rotor in Various Flight Conditions

Approximate Relations and Charts for Low-Speed Stability Derivatives of Swept Wings

An Analysis of the Variation With Altitude of Effective Gust Velocity in Convective-Type Clouds

An Investigation of a Thermal Ice-Prevention System for a Cargo Airplane 9: The Temperature of the Wing Leading-Edge Structure as Established in Flight

Compressive strength of 24S-T aluminum-alloy flat panels with longitudinal formed hat-section stiffeners having four ratios of stiffener thickness to skin thickness

Direct-reading design charts for 75S-T aluminum-alloy flat compression panels having longitudinal straight-web Y-section stiffeners

Damping in pitch and roll of triangular wings at supersonic speeds

The effect of tip modification and thermal de-icing air flow on propeller performance as determined from wind-tunnel tests

Tank tests of a 1/10-size model of a hypothetical flying boat with a hull length-beam ratio of 9.0

Tests of a 45 degree sweptback-wing model in the Langley gust tunnel

Tank tests of three types of afterbodies on a flying-boat model with basic hull length-beam ratio of 10.0

Investigation of some factors affecting comparisons of wind-tunnel and flight measurements of maximum lift coefficients for a fighter-type airplane

Effect of landing flaps and landing gear on the spin and recovery characteristics of airplanes

The buckling of a column on equally spaced deflectional and rotational springs

Wing-tunnel investigation of effects of forward movements of transition on section characteristics of a low-drag airfoil with a 0.24-chord sealed plain aileron


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