Browse TRAIL Inventories

Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses

Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses

Use of constant diffuser Mach number as a control parameter for variable-geometry inlets at Mach numbers of 1.8 to 2.0

Effect of ambient-temperature variation on the matching requirements of inlet-engine combinations at supersonic speeds

A review of NACA research through 1954 on boron compounds as fuels for jet aircraft (Project Zip)

A reexamination of the use of simple concepts for predicting the shape and location of detached shock waves

Analysis of coolant flow and pressure requirements for a return-flow turbine rotor blade design using hydrogen, helium, or air as coolant

Analytical investigation of fuel-cooled turbine blades with return-flow type of finned coolant passages

Wind-tunnel investigation at low speeds to determine flow-field characteristics and ground influence on a model with jet-augmented flaps

Weight-strength studies of structures representative of fuselage construction

Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on a 4-percent-thick sweptback-wing-body model and pressure distribution measurements on an inboard aileron

The erosion of meteors and high-speed vehicles in the upper atmosphere

Basic considerations in the combustion of hydrocarbon fuels with air

Limited heat-transfer, drag, and stability results from an investigation at Mach numbers up to 9 of a large rocket-propelled 10 degree cone

Velocity and friction characteristics of laminar viscous boundary-layer and channel flow over surfaces with ejection or suction

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


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