Browse TRAIL Inventories

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

Methods for obtaining desired helicopter stability characteristics

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

Altitude investigation of can-type flame holder in 20-inch-diameter ram-jet combustor

The transonic aerodynamic characteristics of structurally related wings of low aspect ratio having a spanwise variation in thickness ratio-transonic bump technique

Altitude performance characteristics of the J73-GE-1A turbojet engine

Altitude performance of compressor, turbine, and combustor components of 600-B9 turbojet engine

Altitude performance of compressor, combustor, and turbine components of XT38-A-2 turboprop engine

Altitude-wind-tunnel investigation of several afterburner configurations having moderately high burner-inlet velocities

Additional fatigue tests on effects of design details in 355-T6 sand-cast aluminum alloy

Aerodynamic characteristics at Mach number of 2.01 of two cruciform missile configurations having 70 degree delta wings with length-diameter ratios of 14.8 and 17.7 with several canard controls

The transonic characteristics of unswept wings having aspect ratios of 4, spanwise variations in thickness ratio, and variations in plan-form taper-transonic-bump technique

Tooth-type noise-suppression devices on a full-scale axial-flow turbojet engine

Low-speed measurement of static stability and damping derivatives of a 60 degree delta-wing model for angles of attack of 0 degrees to 90 degrees

Low-velocity turning as a means of minimizing boundary-layer accumulations resulting from secondary flows within turbine stators

Methods of predicting helicopter stability

Sea-level static equilibrium performance of actual two-spool turbojet engine and comparison with hypothetical engine

Rocket-powered-model investigation of the effects of aeroelasticity on the rolling effectiveness of an 8.06-percent-scale McDonnell F3H-1 airplane wing at Mach numbers from 0.5 to 1.4 : TED No. NACA DE 351

Performance comparisons of Navy jet mix and MIL-F-5624A (JP-3) fuels in tubular and annular combustors / Richard J. McCafferty

Preliminary investigation of an asymmetric swept nose inlet of circular projection at Mach number 3.85

Preliminary investigation of pumping and thrust characteristics of full-size cooling-air ejectors at several exhaust-gas temperatures

Stability characteristics at low speed of a variable-sweep airplane model having a partially cambered wing with several chord-extension configurations

An assessment of the airplane drag problem at transonic and supersonic speeds

Aspects of internal-flow-system design for helicopter propulsive units

Influence of combustion-chamber length on afterburner performance

Forces and moments on inclined bodies at Mach numbers from 3.0 to 6.3

Calibration of strain-gage installations in aircraft structures for the measurement of flight loads

Engine performance of alloy 73J turbine blades cast to predetermined grain sizes

Effect of immersed surfaces in combustion zone on efficiency and stability of 5-inch diameter ram-jet combustor

Forced-convection heat-transfer and pressure-drop characteristics of a closely spaced wire matrix

A flight investigation at transonic speeds of the aerodynamic characteristics of a model having a thin unswept wing of aspect ratio 3.1

A flight investigation at transonic speeds and small angles of attack of the aerodynamic characteristics of a model having a 45 degree sweptback wing of aspect ratio 3 with an Naca 64A006 airfoil section

Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) V : aerodynamic load distributions for a series of four boattailed bodies

Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) IV : aerodynamic characteristics of series of four bodies having near-parabolic noses and cylindrical afterbodies

Forced-convection heat-transfer characteristics of molten Flinak flowing in an Inconel system

Investigation of several double-ramp side inlets

The effect of stick-force gradient and stick gearing on the tracking accuracy of a fighter airplane

An experimental investigation of the flutter of several wings of varying aspect ratio, density, and thickness ratio at Mach numbers from 0.60 to 1.10

Experimental investigation of an axial-flow compressor inlet stage operating at transonic relative inlet Mach numbers IV : stage and blade-row performance of stage with axial-discharge stators

Evaluation at supersonic speeds of twin-duct side-intake system with two-dimensional double-shock inlets

Preliminary investigation of the 'freeze-casting' method for forming refractory powders

A preliminary investigation of the use of circulation control to increase the lift of a 45 degree sweptback wing by suction through trailing-edge slots

Kinetic study of mass transfer by sodium hydroxide in nickel under free-convection conditions /by Don R. Mosher and Robert A. Lad


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