Browse TRAIL Inventories

A variational theorem for creep with applications to plates and columns

Thermal relations for two-phase expansion with phase equilibrium and example for combustion products of boron-containing fuel

On flow of electrically conducting fluids over a flat plate in the presence of a transverse magnetic field

Investigation of the compressive strength and creep of 7075-T6 aluminum-alloy plates at elevated temperatures

Investigation of deflectors as gust alleviators on a 0.09-scale model of the Bell X-5 airplane with various wing sweep angles from 20 degrees to 60 degrees at Mach numbers from 0.40 to 0.90

Free-flight investigation to determine some effects of tail damping and wing-tail interference on the rolling effectiveness of ailerons and a spoiler on a modified-delta wing at Mach numbers from 0.6 to 1.5

Material compatibility with gaseous fluorine

Ditching investigations of dynamic models and effects of design parameters on ditching characteristics

Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study 3: experimental performance with two stator configurations designed to eliminate blade wakes and secondary-flow effects and conclusions from entire sta

Performance of a supersonic ramp-type side inlet with ram-scoop throat bleed and varying fuselage boundary-layer removal : Mach number range 1.5 to 2.0

Permeability variation of a taper-rolled wire cloth

A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures

Investigation at low speeds of deflectors and spoilers as gust alleviators on a model of the Bell X-5 airplane with 35 degree swept wings and on a high-aspect-ratio 35 degree swept-wing-fuselage model

Investigation of conditions for spontaneous ignition and combustion efficiency of pentaborane in a small-scale combustor

Charts for estimating the effects of short-period stability characteristics on airplane vertical-acceleration and pitch-angle response in continuous atmospheric turbulence

Effect of fuselage length and a canopy on the static longitudinal and lateral stability characteristics of 45 degrees sweptback airplane models having fuselages with square cross sections

The effect of body contouring on the longitudinal characteristics at Mach numbers up to 0.92 of a wing-fuselage-tail and several wing-fuselage combinations having sweptback wings of relatively high aspect ratio

Effect of burner design variables on performance of 16-inch diameter ram-jet combustor using gaseous-hydrogen fuel

Fatigue-crack propagation and residual static strength of built-up structures

An investigation of discharge and thrust characteristics of flapped outlets for stream Mach numbers from 0.40 to 1.30

Charts for the analysis of flow in a whirling duct

Investigation of effectiveness of a wing equipped with a 50-percent-chord sliding flap, a 30-percent-chord slotted flap, and a 30-percent-chord slat in deflecting propeller slipstreams downward for vertical take-off

External interference effects of a flow through static-pressure orifices of a NACA airspeed head at a Mach number of 3

Ground simulator studies of the effects of valve friction, stick friction, flexibility, and backlash on power control system quality

Experimental investigation of the simulation of atmospheric entry of ballistic missiles

Effects of airplane flexibility on wing bending strains in rough air

The effects of boundary-layer separation over bodies of revolution with conical tail flares

Effects of airplane flexibility on wing strains in rough air at 5,000 feet as determined by flight tests of a large swept-wing airplane

Effects of blade plan form on free-space oscillating pressures near propellers at flight Mach numbers to 0.72

Free-flight investigation of jet effects at low supersonic Mach numbers on a fighter-type configuration employing a tail-boom assembly: longitudinal stability and trim

Free-flight investigation at transonic speeds of the power-on characteristics including some effects of sonic propulsive jets of a four-engine delta-wing configuration

Free-flight investigation of comparative zero-lift rolling effectiveness of a leading edge and a trailing edge air-jet spoiler on an unswept wing

Tensile properties of Inconel X sheet under rapid-heating and constant-temperature conditions

Tensile stress-strain properties of 17-7 PH and AM 350 stainless-steel sheet at elevated temperatures

Chemical igniters for starting jet fuel - nitric acid rockets

A simplified method for assessing the effect of steady rolling on angle of attack and sideslip

A theoretical and experimental study of planing surfaces including effects of cross section and plan form

On possible similarity solutions for three-dimensional incompressible laminar boundary layers 3: similarity with respect to stationary polar coordinates for small angle variation

An investigation at low speed of the flow over a simulated flat plate at small angles of attack using pitot-static and hot-wire probes

A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry

Cascade investigation of a related series of 6-percent-thick guide-vane profiles and design charts

Basic performance characteristics of several subsonic-diffuser-bypass-duct combinations for use with supersonic inlets

Two-dimensional cascade tests of NACA 65-(C(sub zeta)(sub o))A(sub 10))10 blade sections at typical compressor hub conditions for speeds up to choking

Preliminary investigation of dynamic lateral stability characteristics of a configuration of the North American X-15 research airplane

Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute

A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9

Theoretical rocket performance of JP-4 fuel with mixtures of liquid ozone and fluorine

Temperature measurements from a flight test of two wing-body combinations at 7 degree angle of attack for Mach numbers to 4.86 and Reynolds numbers to 19.2 X 10(exp 6)

Investigation of the planing lift of a flat plate at speeds up to 170 feet per second

Effect of bluntness on transition for a cone and a hollow cylinder at Mach 3.1


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