Browse TRAIL Inventories

Interaction of grids with traveling shock waves

Initial results of a flight investigation of a gust-alleviation system

Investigation of plastic behavior of binary aluminum alloys by internal-friction methods

A method for obtaining statistical data on airplane vertical velocity at ground contact from measurements of center-of-gravity acceleration

The nickel dip : a radioisotope study of metallic deposits in porcelain enameling

Preliminary study of some factors which affect the stall-flutter characteristics of thin wings

Lift and moment coefficients for an oscillating rectangular wing-aileron configuration in supersonic flow

Measurement of aerodynamic forces for various mean angles of attack on an airfoil oscillating in pitch and on two finite-span wings oscillating in bending with emphasis on damping in the stall

Heat capacity lag of gaseous mixtures

Further measurements of intensity, scale, and spectra of turbulence in a subsonic jet

Effect of combustion-chamber pressure and nozzle expansion ratio on theoretical performance of several rocket propellant systems

The design of a miniature solid-propellant rocket

Effect of phosphate coatings on temperature of metal parts exposed to flame environments

Effect of pneumatic de-icers and ice formations on aerodynamic characteristics of a airfoil

Analytical study of modifications to the autopilot of a fighter airplane in order to reduce the response to side gusts

Comparison of landing-impact velocities of first and second wheel to contact from statistical measurements of transport airplane landings

Compressibility factor, density, specific heat, enthalpy, entropy, free-energy function, viscosity, and thermal conductivity of steam

Compressive crippling of structural sections

An analysis of estimated and experimental transonic downwash characteristics as affected by plan form and thickness for wing and wing-fuselage configurations

Experimental and calculated temperature and mass histories of vaporizing fuel drops

Results of axial-load fatigue tests on electropolished 2024-T3 and 7075-T6 aluminum-alloy-sheet specimens with central holes

Properties of aircraft fuels

Performance of a Double-Ramp Side Inlet With Combinations of Fuselage, Ramp, and Throat Boundary-Layer Removal, Mach Number Range, 1.5 to 2.0

Performance of Pentaborane, Pentaborane - JP-4 Fuel Mixtures, and Trimethylborate Azeotrope Fuel in a Full-scale Turbojet Engine

Performance of Several Half-Conical Side Inlets at Supersonic and Subsonic Speeds

Performance of Variable Two-Dimensional Inlet Designed for Engine-Inlet Matching 1 - Performance at Design Mach Number of 3.07

Some Effects of Roll Rate on the Longitudinal Stability Characteristics of a Cruciform Missile Configuration as Determined From Flight Test for a Mach Number Range of 1.1 to 1.8

Some Transonic Aerodynamic Characteristics of a Model Similar to the McDonnell F3H-2N Airplane

Static Lateral and Directional Stability and Control Characteristics of a Revised 1/22-Scale Model of the Republic F-105 Airplane at Mach Numbers of 1.41 and 2.01

Preliminary Report on Experimental Investigation of Engine Dynamics and Controls for a 48-Inch Ramjet Engine

Preliminary Investigation of the Static Longitudinal and Lateral Stability Characteristics of a 1/20-Scale Model of the McDonnell F4H-1 Airplane at Mach Numbers of 1.59, 1.89, and 2.09

Surge-Inception Study in a Two-Spool Turbojet Engine

Transonic Aerodynamic Characteristics of a 1/15-Scale Model of the Convair B-58 Airplane

Static Longitudinal and Lateral Stability Characteristics Including Effects of Transonic Area Rule and Wing Modification of a 0.10- Scale Model of the Douglas A4D-1 Airplane at Transonic Speeds

Some Flight Data for the Chance Vought Regulus 2 Missile

Wind Tunnel Investigation at High Subsonic Speeds of Drag at 0 Degrees Angle of Attack of Swept-Wing Fuselage Models With Pylon Mounted and Semisubmerged Missiles

Wind Tunnel Investigation at Low Speed of Aerodynamic Characteristics of Army Chemical Corps Model E-112 Bomblets with Span Chord Ratio of 2 - 1

An Airborne Simulator Investigation of the Accuracy of an Optical Track Command Missile Guidance System

Tests With Hydrogen Fuel in a Simulated Afterburner

Thermal Stability of Decaborane and of a Commercial Ethyl Decaborane (HEF-3) in the Range 202 Degrees to 252 Degrees C

An Oil-Stream Photomicrographic Aeroscope for Obtaining Cloud Liquid-Water Content and Droplet Size Distributions in Flight

Experimental Droplet Impingement on Several Two-Dimensional Airfoils with Thickness Ratios of 6 to 16 Percent

Drag at Model Trim Lift of a 1/15-Scale Convair B-58 Supersonic Bomber

Low-Speed Investigation of the Effect of Small Canard Surfaces on the Directional Stability of a Sweptback-Wing Fighter-Airplane Model

Pressure Distributions and Aerodynamic Characteristics of Several Spoiler-type Controls on a Trapezoidal Wing at Mach Numbers of 1.61 and 2.01

Presentation on Facility Problems in High-Temperature Structures Research

Effect of Combustion Gas Properties on Turbojet-Engine Performance With Hydrogen as Fuel

Experimental Investigation of a High Subsonic Mach Number Turbine Having High Rotor Blade Suction-Surface Diffusion

Force and Pressure-Distribution Investigation to High Angles of Attack on All-Movable Triangular and Rectangular Wings in Combination With a Body at Supersonic Speeds

Full-Scale Wind-Tunnel Tests of a 35 Degree Swept-Wing Fighter Airplane With a Spoiler-Slot-Deflector Lateral Control System


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