Browse TRAIL Inventories

Static crucible investigation of corrosion and mass-transfer of nickel in molten sodium hydroxide with various additives

Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds

Tests in the Ames 40- by 80-foot wind tunnel of two airplane models having aspect ratio 2 trapezoidal wings of taper ratios 0.33 and 0.20

Experimental investigation of aerodynamically balanced trailing-edge control surfaces on an aspect ratio 2 triangular wing at subsonic and supersonic speeds

An experimental study of porosity characteristics of perforated materials in normal and parallel flow

The effect at high subsonic speeds of a flap-type aileron on the chordwise pressure distribution near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil section

The effects of extensible rocket racks on lift, drag, and stability of a 1/10-scale rocket-boosted model of the McDonnell XF3H-1 airplane for a Mach number range of 0.60 to 1.34 : TED No. NACA DE 31

Effects of high degrees of biaxial stretch forming on crazing and other properties of acrylic plastic glazing

Effects of nitrogen tetroxide and water concentration on freezing point and ignition delay of fuming nitric acid

Comparison of ignition delays of several propellant combinations obtained with modified open-cup and small-scale rocket engine apparatus

Ignition delays of alkyl thiophosphites with white and red fuming nitric acids within temperature range 80 to -105 degrees Fahrenheit

A flight investigation of the effect of leading-edge camber on the aerodynamic characteristics of a swept-wing airplane

Investigation of 16-inch impulse-type supersonic compressor rotor with turning past axial direction

Investigation at transonic speeds of aerodynamic characteristics of a semielliptical air inlet in the root of a 45 degree sweptback wing

A theory for stability and buzz pulsation amplitude in ram jets and an experimental investigation including scale effects

Use of flame-immersed blades to improve combustion limits and efficiency of a 5-inch diameter connected-pipe, ram-jet combustor

Subsonic static longitudinal stability and control characteristics of a wing-body combination having a pointed wing of aspect ratio 2 with constant-percent-chord trailing-edge elevons

A summary of data on the division of loads for various wing-fuselage combinations

A transonic wind-tunnel investigation of the effects of body indentation, as specified by the transonic drag-rise rule, on the aerodynamic characteristics and flow phenomena of a 45 degree sweptback-wing-body combination

Turbine design considerations for turbine-propeller engine operating over a range of flight conditions

Turbojet-engine thrust augmentation at altitude by combined ammonia injection into the compressor inlet and afterburning

A transonic wind-tunnel investigation of the longitudinal stability and control characteristics of a 0.09-scale model of the Bell X-5 research airplane and comparison with flight

Altitude investigation of XJ34-WE-32 engine performance without electronic control

Altitude operational characteristics of prototype J40-WE-8 turbojet engine

Altitude evaluation of several afterburner design variables on a J47-GE-17 turbojet engine

Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds: taper-ratio series

Wind-tunnel investigation of stall control by suction through a porous leading edge on a 37 degree sweptback wing of aspect ratio 6 at Reynolds numbers from 2.50 x 10(exp 6) to 8.10 x 10(exp 6)

Altitude performance investigation of a high-temperature afterburner

Altitude performance investigation of two single-annular type combustors and the prototype J40-WE-8 turbojet engine combustor with various combustor-inlet air pressure profiles

Altitude performance of a 20-inch-diameter ram-jet engine investigated in a free jet facility at Mach number 3.0

Altitude performance characteristics of the J47-25 turbojet engine: data presentation

Aerodynamic characteristics at Mach number 4.04 of a rectangular wing of aspect ratio 1.33 having a 6-percent-thick circular-arc profile and a 30-percent-chord full-span trailing-edge flap

Adhesive and protective characteristics of ceramic coating A-417 and its effect on engine life of forged Refractaloy-26 (AMS 5760) and cast stellite 21 (AMS 5385) turbine blades

A theoretical study of the effect of control-deflection and control-rate limitations on the normal acceleration and roll response of a supersonic interceptor

Transonic aerodynamic characteristics of an NACA 64A006 airfoil section with a 15-percent-chord leading-edge flap.

Theoretical study of the tunnel-boundary lift interference due to slotted walls in the presence of the trailing-vortex system of a lifting model

Low-speed, large-scale investigation of aerodynamic characteristics of a semispan 49 degree sweptback wing with a Fowler flap in combination with a plain flap, slats, and fences

Low-speed lateral control characteristics of an unswept wing with hexagonal airfoil sections and aspect ratio 4.0 at a Reynolds number of 6.2 x 10(exp 6)

Low-speed wind-tunnel investigation of a thin 60 degree delta wing with double slotted, single slotted, plain, and split flaps

Low-speed static stability and control characteristics of a 1/4-scale model of the Bell X-1 airplane equipped with a 4-percent-thick, aspect-ratio-4, unswept wing

Investigation of the use of a stick force proportional to pitching acceleration for normal-acceleration warning

Minimum spark-ignition energies of 12 pure fuels at atmospheric and reduced pressure

Prediction of flame velocities of hydrocarbon flames

The Sodium Hydroxide Reactor : Effect of Reactor Variables on Criticality and Fuel-Element Temperature Requirements for Subsonic and Supersonic Aircraft Nuclear Propulsion

Some approximate methods for estimating the effects of aeroelastic bending of rocket-propelled model-booster combinations

Smoke studies of secondary flows in bends, tandem cascades, and high-turning configurations

Model ditching investigations of three airplanes equipped with hydro-skis

Performance comparison at supersonic speeds of inlets spilling excess flow by means of bow shock, conical shock, or bypass

Performance comparison of three canard-type ram-jet missile configurations at Mach numbers from 1.5 to 2.0

Preliminary investigation of plate-type molybdenum disilicide fuel elements for an air-cycle nuclear reactor


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