Browse TRAIL Inventories

Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading

Use of a diffuser Mach number as a supersonic-inlet control parameter

Low-speed measurements of static stability, damping in yaw, and damping in roll of a delta, a swept, and an unswept wing for angles of attack from 0 degrees to 90 degrees

Low-speed pressure-distribution investigation of a spoiler and a spoiler-slot-deflector on a 30 degree sweptback wing-fuselage model having an aspect ratio of 3, a taper ratio of 0.5, and NACA 65A004 airfoil section

Low-speed pressure-distribution investigation of a thin-delta-wing-fuselage model with double slotted flap, extended double slotted flap, and canard

Low-speed measurements of tail contribution to rolling stability derivatives and air-flow angularity at the tail for an x-tail model in steady roll including some effects of wing-tip stores

Low-speed investigation of the lateral-control characteristics of a flap-type spoiler and a spoiler-slot deflector on a 30 degree sweptback wing-fuselage model having an aspect ratio of 3, a taper ratio of 0.5, and NACA 65A004 airfoil section

Low-Speed Static Stability Characteristics of a Complete Model with an M-Wing in Mid and High Positions and with Three Horizontal-Tail Heights

Low-speed wind-tunnel results for a thin aspect-ratio-1.85 pointed-wing-fuselage model with double slotted flaps

Methods for measuring temperatures of thin-walled gas-turbine blades

Methods for calculating thrust augmentation and liquid consumption for various turbojet-afterburner fuels

Minimum-drag ducted and closed three-point body of revolution based on linearized supersonic theory

Minimum drag of the Chance Vought XF8U-1 airplane as determined from the flight test of a 0.11-scale rocket-boosted model at Mach numbers between 0.73 and 1.71 : TED No. NACA DE 392

Motion of a ballistic missile angularly misaligned with the flight path upon entering the atmosphere and its effect upon aerodynamic heating, aerodynamic loads, and miss distance

Instrumentation for measurements of free-space sound pressures in the immediate vicinity of a propeller in flight

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


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