Browse TRAIL Inventories

Design and experimental investigation of a single-stage turbine with a downstream stator

Design and test of mixed-flow impellers 8: comparison of experimental results for three impellers with shroud redesigned by rapid approximate method

The interrelated effects of engine rotor momentum and flight regime on the dynamic stability of high-performance aircraft

Effects of vertical location of wing and horizontal tail on the aerodynamic characteristics in pitch at Mach numbers from 0.60 to 1.40 of an airplane configuration with an unswept wing

Effects of wing-mounted external stores on the longitudinal and lateral handing qualities of the Douglas D-558-II research airplane

Effects of wing warp on the lift, drag, and static longitudinal stability characteristics of an aircraft configuration having an arrow wing of aspect ratio 1.86 at Mach numbers from 1.1 to 1.7

Analysis of shock motion in ducts during disturbances in downstream pressure

A hydrogen peroxide turbojet-engine simulator for wing-tunnel powered-model investigations

Experimental investigation of dynamic relations in a 48-inch ram-jet engine

The application of matrix methods to coordinate transformations occurring in systems studies involving large motions of aircraft

An analog computer study of several stability augmentation schemes designed to alleviate roll-induced instability

Application of obliquely mounted strain gage to measurement of residual stresses in disks

A balanced-pressure sliding seal used for transfer of pressurized air between stationary and rotating parts

Base pressure at supersonic speeds on two-dimensional airfoils and on bodies of revolution with and without fins having turbulent boundary layers

Investigation of semivaneless turbine stator designed to produce axially symmetrical free-vortex flow

Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study 2: design and experimental performance of turbine with low-velocity-turning stator and standard rotor

Jet effects on base pressures of conical afterbodies at Mach 1.91 and 3.12

Static longitudinal and lateral stability characteristics at low speed of 45 degree sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6

Wind-tunnel investigation of external-flow jet-augmented double slotted flaps on a rectangular wing at an angle of attack of 0 degree to high momentum coefficients

Wind-tunnel investigation of effect of propeller slipstreams on aerodynamic characteristics of a wing equipped with a 50-percent-chord sliding flap and a 30-percent-chord slotted flap

Wind-tunnel investigation of effects of ground proximity and of split flaps on the lateral stability derivatives of a 60 degree delta-wing model oscillating in yaw

Some experiments at high supersonic speeds on the aerodynamic and boundary-layer transition characteristics of high-drag bodies of revolution

Investigation of boundary-layer transition on flat-faced bodies of revolution at high supersonic speeds

Performance comparison at Mach numbers 1.8 and 2.0 of full-scale and quarter-scale translating-spike inlets

Analysis of two-stage-turbine efficiency characteristics in terms of work and speed requirements

Analysis of efficiency characteristics of a single-stage turbine with downstream stators in terms of work and speed requirements

Investigation of a supersonic-inlet - turbojet-engine combination at Mach 2.0 and angles of attack up to 6 degrees

Use of main-inlet bypass to supply ejector exhaust nozzle at supersonic speeds

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


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