TRAIL - Technical Report Archive and Image Library

Effect of wing slats and inboard wing fences on the longitudinal stability characteristics of the DOUGLAS D-558-II airplane in accelerated maneuvers at subsonic and transonic speeds

Effects of leading-edge chord extensions and an all-movable horizontal tail on the aerodynamic characteristics of a wing-body combination employing a triangular wing of aspect ratio 3 mounted in a high position at subsonic and supersonic speeds

Effects of multiaxial stretching on crazing and other properties of transparent plastics

Effects of molecular weight on crazing and tensile properties of polymethyl methacrylate

Effectiveness of boundary-layer removal near throat of ramp-type side inlet at free-stream Mach number of 2.0

Effect on transonic and supersonic drag of fuselage gloves designed to give a smooth overall area distribution to a swept-wing--body combination

Effect on the low-speed aerodynamic characteristics of a 49 degree sweptback wing having an aspect ratio of 3.78 of blowing air over the trailing-edge flap and aileron

Evaluation of Altitude-Ignition Characteristics of Three Fuels of Different Volatility in a Turbojet Engine

Effects of two spinner shapes on the pressure recovery in an NACA 1-series D-type cowl behind a three-blade propeller at Mach numbers up to 0.80

Experimental determination of boundary-layer transition on a body of revolution at M = 3.5

Experimental data for four full-scale conical cooling-air ejectors

Experimental determination of aerodynamic forces normal to the chord due to rotating stall acting on compressor blading

An experimental investigation of four triangular-wing-body combinations in sideslip at Mach numbers 0.6, 0.9, 1.4, and 1.7

Experimental investigation of control signals and the nature of stall and surge behavior in a turbojet engine

Experimental investigation of effect of high-aspect-ratio rotor blades on performance of conservatively designed turbine

Experimental investigation of the effect of a shrouded rotor on the performance of a conservatively designed turbine

Experimental investigation of the effect of fuel-injection-system design variables on afterburner performance

Experimental investigation of the aerodynamic characteristics of a ballistic-type missile

Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a 52.5 degree delta wing and a low, swept horizontal tail

Aerodynamic characteristics including effects of wing fixes of a 1/20-scale model of the Convair F-102 airplane at transonic speeds

Aerodynamic characteristics of a cruciform-wing missile with canard control surfaces and of some very small span wing-body missiles at a Mach number of 1.41

Aerodynamic characteristics of a full-span trailing-edge control on a 60 degree delta wing with and without a spoiler at Mach number 1.61

Effect of inlet-annulus area blockage on over-all performance and stall characteristics of an experimental 15-stage axial-flow compressor

Multiple over-all performance and rotating-stall characteristics of a 15-stage experimental axial-flow compressor at an intermediate speed

Summary of rocket-model tests at zero lift of an arrow-wing missile configuration from Mach numbers of 0.9 to 1.8

Results of free-flight test of 1/10-scale model of the Convair XF2Y-1 airplane between Mach numbers of 0.7 and 1.45, including power-on flight at Mach number 1.2 : TED No. NACA DE 365

Shock-turbulence interaction and the generation of noise

Some screeching-combustion characteristics of a transpiration-cooled afterburner having a porous wall of wire cloth

Some observations of shock-induced turbulent separation on supersonic diffusers

Some internal-flow characteristics of several axisymmetrical NACA 1-series nose air inlets at zero flight speed

Starting and performance characteristics of a large asymmetric supersonic free-jet facility

Starting characteristics and combustion performance of magnesium slurry in 6.5-inch-diameter ram-jet engine mounted in connected-pipe facility

Pumping and thrust characteristics of several divergent cooling-air ejectors and comparison of performance with conical and cylindrical ejectors

Tests in the Ames 40- by 80-foot wind tunnel of the aerodynamic characteristics of airplane models with plain spoiler ailerons

The effects of wing-mounted external stores on the trim, buffet, and drag characteristics of a rocket-propelled model having a 45 degree sweptback wing

Experimental performance of liquid fluorine-liquid ammonia propellant combination in 1000-pound-thrust rocket engines

Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of a spoiler-slot-deflector control located at two spanwise positions

Effects of high-lift devices and horizontal-tail location on the low-speed characteristics of a large-scale 45 degree swept-wing airplane configuration

Investigation of the effects of profile shape on the aerodynamic and structural characteristics of thin, two-dimensional airfoils at supersonic speeds

Flight investigation of the effects of horizontal-tail height, moment of inertia, and control effectiveness on the pitch-up characteristics of a 35 degree swept-wing fighter airplane at high subsonic speeds

Flight investigation of the effects of a partial-span leading-edge chord extension on the aerodynamic characteristics of a 35 degree swept-wing fighter airplane

Free-flight measurements of the rolling effectiveness and operating characteristics of a bellows-actuated split-flap aileron on a 60 degree delta wing at Mach numbers between 0.8 and 1.8

Summary of free-flight performance of a series of ram-jet engines at Mach numbers from 0.80 to 2.20

Investigation of a 1/4-scale model of the Republic F-105 airplane in the Langley 19-foot pressure tunnel : influence of trailing-edge flap span and deflection on the longitudinal characteristics

Investigation of a 1/4-Scale Model of the Republic F-105 Airplane in the Langley 19-Foot Pressure Tunnel: Longitudinal Stability and Control of the Model Equipped with a Supersonic-Type Elliptical Wing-Root Inlet

Transonic wind-tunnel investigation of the effect of body indentation for boattail and cylindrical afterbody shapes on the aerodynamic characteristics of an unswept-wing-body combination

A transonic wind-tunnel investigation of the effects of twist and camber with and without incidence, twist and body indentation on the aerodynamic characteristics of a 45 degree sweptback wing-body configuration

A summary of information on support interference at transonic and supersonic speeds

Altitude performance and operational characteristics of an XT38-A-2 turboprop engine

Altitude-chamber investigation of J73-GE-1A turbojet engine component performance

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