Browse TRAIL Inventories

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

A study of the radiation from laminar and turbulent open propane-air flames as a function of flame area, equivalence ratio, and fuel flow rate

Study of the physical properties of petrolatum-stabilized magnesium-hydrocarbon slurry fuels

Study of the attack of an automatically controlled interceptor on a maneuvering bomber with emphasis on proper coordination of lift-acceleration and roll-angle commands during rolling maneuvers

Preliminary performance data for the J57-P-1 turbojet engine at altitudes up to 65,000 feet

A revised gust-load formula and a re-evaluation of v-g data taken on civil transport airplanes from 1933 to 1950

Rocket-model investigation of the longitudinal stability and drag characteristics of a 1/10-scale model of the Convair XF2Y-1 airplane having open ducts and the elevons deflected upward 3.5 degrees : TED No. NACA DE 375

Analytical and experimental studies of a divided-flow ram-jet combustor

Analysis of the turbojet for propulsion of supersonic bombers

Analytical determination of effect of turbine cooling-air-impeller performance on engine performance and comparison of experimentally determined performance of impellers with and without inducer vanes

Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio - transonic bumb method

Experimental heat-transfer and friction coefficients for air flowing through stacks of parallel flat plates

Experimental influence coefficients for the deflection of the wing of a full-scale, swept-wing bomber

Impingement of water droplets on wedges and double-wedge airfoils at supersonic speeds

Preliminary investigation of performance of variable-throat extended-plug-type nozzles over wide range of nozzle pressure ratios

An Investigation of the Hydrodynamic Characteristics of a 1/10-Size Powered Dynamic Model of the Martin M-267 Patrol-Type Seaplane with Two Forebody Configurations: TED No. NACA DE 376


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