Browse TRAIL Inventories

Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds

Measurements of pressure and temperature for appraisal of the temperature method of airspeed calibration in the lower stratosphere

Investigation of mutual interference effects of several vertical-tail-fuselage configuration in sideslip

Description and preliminary flight investigation of an instrument for detecting subnormal acceleration during take-off

Boundary-layer transition at Mach 3.12 with and without single roughness elements

An investigation of the use of rocket-powered models for gust-load studies with an application to a tailless swept-wing model at transonic speeds

Considerations on a large hydraulic jet catapult

Preliminary Altitude Performance Characteristics of the J57-P-1 Turbojet Engine with Fixed-Area Exhaust Nozzle

Performance of 15-Stage Experimental J71 Axial-Flow Compressor: 2 - Individual Stage Performance Characteristics

Effect on Drag of Longitudinal Positioning of Half-Submerged and Pylon-Mounted Douglas Aircraft Stores on a Fuselage with and without Cavities between Mach Numbers 0.9 and 1.8

Permeability and Strength Measurements on Sintered, Porous, Hollow Turbine Blades Made by the American Electro Metal Corporation under Office of Naval Research Contract N-ONR-295 (01)

Experimental Permeability Measurements on a Strut-Supported Transpiration-Cooled Turbine Blade with Stainless-Steel Shell made by the Federal-Mogul Corporation under Bureau of Aeronautics Contract N0as 51613-C

Summary of Free-Flight Zero-Lift Drag Results from Tests of 1/5-Scale Models of the Convair YF-102 and F-102A Airplanes and Several Related Small Equivalent Bodies at Mach Numbers from 0.70 to 1.46

Free-Flight Zero-Lift Drag Results from a 1/5-Scale Model and Several Small-Scale Equivalent Bodies of Revolution of the Convair F-102 Configuration at Mach Numbers up to 1.34

A note on secondary flow in rotating radial channels

Determination of mean camber surfaces for wings having uniform chordwise loading and arbitrary spanwise loading in subsonic flow

An analytical study of the effect of airplane wake on the lateral dispersion of aerial sprays

An air-flow-direction pickup suitable for telemetering use on pilotless aircraft

A comparative analysis of the performance of long-range hypervelocity vehicles

Behavior of materials under conditions of thermal stress

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


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