TRAIL - Technical Report Archive and Image Library

Control deflections, airplane response, and tail loads measured on an F-100A airplane in service operational flying

Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively

Simplified method for determination of critical height of distributed roughness particles for boundary-layer transition at Mach numbers from 0 to 5

Effect of temperature on rolling-contact fatigue life with liquid and dry powder lubricants

Experimental investigation of axial and normal force characteristics of skewed nozzles

Experimental investigation of the effects of some shroud design variables on the static thrust characteristics of a small-scale shrouded propeller submerged in a wing

Experimental investigation of an impulse-type supersonic compressor rotor having a turning of 73 degrees at the mean radius

Jet effects on the base drag of a cylindrical afterbody with extended nozzles

Dilution of liquid oxygen when nitrogen is used for pressurization

Performance of an All-Internal Conical Compression Inlet with Annular Throat Bleed at Mach Number 5.0

A numerical method for evaluating wave drag

Physical characteristics and test conditions of an ethylene-heated high-temperature jet

Observations of turbulent-burst geometry and growth in supersonic flow

Some effects of flow spoilers and of aerodynamic balance on the oscillating hinge moments for a swept fin-rudder combination in a transonic wind tunnel

Preliminary performance data obtained in a full-scale, free-jet investigation of a side-inlet supersonic diffuser

Thin airfoil theory based on approximate solution of the transonic flow equation

Wind-tunnel tests of a full-scale helicopter rotor with symmetrical and with cambered blade sections at advance ratios from 0.3 to 0.4

Analytical and experimental investigation of a temperature-schedule acceleration control for a turbojet engine

Analytical and experimental investigation of temperature recovery factors for fully developed flow of air in a tube

Analysis of turbulent flow and heat transfer on a flat plate at high Mach numbers with variable fluid properties

Use of the Coanda effect for obtaining jet deflection and lift with a single flat-plate deflection surface

Use of the Coanda effect for jet deflection and vertical lift with multiple-flat-plate and curved-plate deflection surfaces

Use of the Kernel function in a three-dimensional flutter analysis with application to a flutter-tested delta-wing model

Transonic investigation of yawed wings of aspect ratios 3 and 6 with a Sears-Haack body and with symmetrical and asymmetrical bodies indented for a Mach number of 1.20

Analysis of transonic rotor-blade passage loss with hot-wire anemometers

An analysis of the turbulent boundary-layer characteristics on a flat plate with distributed light-gas injection

An approximate analytical method for studying entry into planetary atmospheres

Turbulent boundary layer on a yawed cone in a supersonic stream

Wind-tunnel investigation of the high-subsonic static longitudinal stability characteristics of several wing-body configurations designed for high lift-drag ratios at a Mach number of 1.4

Wind-tunnel investigation of the static longitudinal stability and trim characteristics of a sweptback-wing jet-transport model equipped with an external-flow jet augmented flap

Flight investigation of the low-speed characteristics of a 45 degree swept-wing fighter-type airplane with blowing boundary-layer control applied to the trailing edge flaps

Experimental investigation of a high subsonic Mach number turbine having a 40-blade rotor with zero suction-surface diffusion

Free-flight roll performance of a steady-flow jet-spoiler control on an 80 degree delta-wing missile between Mach numbers of 0.6 and 1.8

Free-flight transonic model investigation of jet effects on a fighter-type configuration employing a tail boom and three horizontal-tail positions

Investigation of boiling burnout and flow stability for water flowing in tubes

The rate of fatigue-crack propagation in two aluminum alloys

Effect of sliding velocity on friction properties and endurance life of bonded lead monoxide coatings at temperatures up to 1250 F

Collection of zero-lift drag data on bodies of revolution from free-flight investigations

Effects of fabrication-type roughness on turbulent skin friction at supersonic speeds

Effects of fixing boundary-layer transition for an unswept-wing model and an evaluation of porous tunnel-wall interference for Mach numbers from 0.60 to 1.40

Comparison of shock-expansion theory with experiment for the lift, drag, and pitching-moment characteristics of two wing-body combinations at M=5.0

Effect of screens in reducing distortion and diffusion length for a 'dump' diffuser at a Mach number of 3.85

Effect of jet temperature on jet-noise generation

An analysis of surface pressures and aerodynamic load distribution over the swept wing of the Douglas D-558-II research airplane at Mach numbers from 0.73 to 1.73

Application of a high-temperature static strain gage to the measurement of thermal stresses in a turbine stator vane

Application of statistical theory to beam-rider guidance in the presence of noise 2: modified Wiener filter theory

Measurements of total hemispherical emissivity of various oxidized metals at high temperature

Measurements of ground-reaction forces and vertical center-of-gravity accelerations of a bomber airplane taxiing over obstacles

Study of ground-reaction forces measured during landing impacts of a large airplane

Wind-tunnel investigation of effects of spoiler location, spoiler size, and fuselage nose shape on directional characteristics of a model of a tandem-rotor helicopter fuselage

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