TRAIL - Technical Report Archive and Image Library

Free-spinning-tunnel investigation to determine the effect of spin-recovery rockets and thrust simulation on the recovery characteristics of a 1/25-scale model of the Chance Vought XF8U-1 airplane: TED No. NACA DE 392

The effects of flexibility on the longitudinal and lateral directional response of a large airplane

A comparison of the maneuvering performance of a monowing versus a cruciform missile

The effect of leading-edge droop upon the pressure distribution and aerodynamic loading characteristics of a 45 degree sweptback wing at transonic speeds

The effect of blunt-trailing-edge elevons on the longitudinal and lateral handling qualities of the semitailless airplane

Effect of rotor leading-edge sweepback on performance of a transonic turbine

Description and bibliography of NACA research on wing controls: January 1946 - February 1955

Design and performance of a 1400-foot-per-second-tip-speed supersonic compressor rotor

Effects of spanwise location of sweep discontinuity on the low-speed longitudinal stability characteristics of a complete model with wings of M and W plan form

Effects of spanwise location of sweep discontinuity on the low-speed static lateral stability characteristics of a complete model with wings of M and W plan form

A method for evaluating the loads and controllability aspects of the pitch-up problem

Application of non-afterburning turbojets to supersonic flight

Application of statistical theory to beam-rider guidance in the presence of noise 1: Wiener filter theory

Application of wing-body theory to drag reduction at low supersonic speeds

Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 2

Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 1.98

Wind-tunnel investigation at Mach 1.9 of multijet-missile base pressures

Performance of four experimental high btu-per-gallon fuels in a single turbojet combustor

Performance of a supersonic compressor with swept and tilted diffuser blades

Matching of auxiliary inlets to secondary-air requirements of aircraft ejector exhaust nozzles

Some design implications of the effects of aerodynamic heating

Spark ignition of flowing gases 5: application of fuel-air-ratio and initial-temperature data to ignition theory

A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds

Panel-flutter investigation at supersonic speeds of a pressurized structure fabricated of 0.020-inch-thick laminated glass-plastic

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines 4: coolant-flow requirements and performance of engines using air-cooled corrugated-insert blades

Analytical comparison of convection-cooled turbine blade cooling-air requirements for several radial gas-temperature profiles

Wind-tunnel investigation at low speed of a wing having 63 degree sweepback and a drooped tip

Performance characteristics of axisymmetric two-cone and isentropic nose inlets at Mach number 1.90

A variable-geometry axisymmetric supersonic inlet with telescoping centerbody

Downwash survey behind two low-aspect-ratio variable-incidence wings in combination with three different size fuselages at a Mach number of 0.25

Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase

Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic speeds

A study of conical camber for triangular and sweptback wings

Investigation of effectiveness of large-chord slotted flaps in deflecting propeller slipstreams downward for vertical take-off and low-speed flight

Lift, drag, and longitudinal stability at Mach numbers from 1.4 to 2.3 of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces

Transportation of liquid fluorine

Analysis of Low-Temperature Nuclear-Powered Ram-Jet Missile for High Altitudes

Model investigation of the effect of mounting hydro-skis on shock absorbers

Lift, drag, and longitudinal stability at Mach numbers from 0.8 to 2.1 of a rocket-powered model having a tapered unswept wing of aspect ratio 3 and inline tail surfaces

Performance characteristics of hemispherical target-type thrust reversers

Performance of YJ73-GE-3 turbojet engine in altitude test chamber

Investigation at high subsonic speeds of the effects of various underwing external-store arrangements on the aerodynamic characteristics of a 1/16-scale model of the Douglas D-558-II Research Airplane

An investigation at high subsonic speeds of the effects of horizontal-tail height on the aerodynamic and loading characteristics in sideslip on a 45 degree sweptback, untapered tail assembly as determined from force tests and integrated vertical-tail span loadings

The effect of fluid injection on the compressible turbulent boundary layer : preliminary tests on transpiration cooling of a flat plate

Effect of fuselage fences on the angle-of-attack supersonic performance of a top-inlet-fuselage configuration

A theoretical analysis of the effect of engine angular momentum on longitudinal and directional stability in steady rolling maneuvers

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