Browse TRAIL Inventories

Bonded lead monoxide films as solid lubricants for temperatures up to 1250 F

Boundary-layer transition at Mach 3.12 as affected by cooling and nose blunting

Effect of overheating on creep-rupture properties of S-816 alloy at 1,500 F

Expected numbers of maxima and minima of a stationary random process with non-Gaussian frequency distribution

Experimental and calculated histories of vaporizing fuel drops

Wind-tunnel technique for simultaneous simulation of external flow field about nacelle inlet and exit airstreams at supersonic speeds

Design and experimental evaluation of a light-weight turbine-wheel assembly

Effects of leading-edge blunting on the local heat transfer and pressure distributions over flat plates in supersonic flow

The effect of forward-flight speed on the propulsive characteristics of a pulse-jet engine mounted on a helicopter rotor

Effect of frequency and temperature on fatigue of metals

Effect of propeller location and flap deflection on the aerodynamic characteristics of a wing-propeller combination for angles of attack from 0 degrees to 80 degrees

Effects of thermal relaxation and specific-heat changes on measurements with a pneumatic-probe pyrometer

Experimental investigation of several afterburner configurations on a J79 turbojet engine

The use of pure twist for drag reduction on arrow wings with subsonic leading edges

Estimation of compressible boundary-layer growth over insulated surfaces with pressure gradient

Estimation of incremental pitching moments due to trailing-edge flaps on swept and triangular wings

Experimental determination at subsonic speeds of the oscillatory and static lateral stability derivatives of a series of delta wings with leading-edge sweep from 30 to 86.5 degrees

Experimental investigation of flow fields at zero sideslip near swept- and unswept-wing-fuselage combinations at low speed

An experimental and theoretical study of the effect of fuel on pitching-translation flutter

Experimental and theoretical aerodynamic characteristics of two low-aspect-ratio delta wings at angles of attack to 50 degrees at a Mach number of 4.07

Experimental investigation of lift, drag, and pitching moment of five annular airfoils

Experimental investigation of cermet turbine blades in an axial-flow turbojet engine

Experimental investigation of deposition by boron-containing fuels in turbojet combustor

Experimental investigation of ejector-nozzle metal temperatures

The aerodynamic characteristics of a body in the two-dimensional flow field of a circular-arc wing at a Mach number of 2.01

Flight measurements of boundary-layer temperature profiles on a body of revolution (NACA RM-10) at Mach numbers from 1.2 to 3.5

Some experimental studies of panel flutter at Mach number 1.3

Supplementary investigation in the Langley 20-foot free-spinning tunnel of a 1/20-scale model of the Douglas F4D-1 airplane with external wing fuel tanks : TED No. NACA AD 3116

Supersonic aerodynamic characteristics of a low-drag aircraft configuration having an arrow wing of aspect ratio 1.86 and a body of fineness ratio 20

Results of an investigation at high subsonic speeds to determine lateral-control and hinge-moment characteristics of a spoiler-slot-deflector configuration on a 35 degree sweptback wing

Propellant vaporization as a criterion for rocket engine design : calculations of chamber length to vaporize a single n-heptane drop

Some Reynolds number phenomena in a turbojet compressor

Some research results on sandwich structures

Studies of structural failure due to acoustic loading

Static lateral characteristics at high subsonic speeds of a complete airplane model with a highly tapered wing having the 0.80 chord line unswept and with several tail configurations

The response of an airplane to random atmospheric disturbances

Results of two free-fall experiments on flutter of thin unswept wings in the transonic speed range

Static longitudinal and lateral stability parameters of three flared-skirt two-stage missile configurations at a Mach number of 6.86

Static-pressure error calibrations for nose-boom airspeed installations of 17 airplanes

Static longitudinal characteristics at high subsonic speeds of a complete airplane model with a highly tapered wing having the 0.80 chord line unswept and with several tail configurations

Propellant vaporization as a criterion for rocket-engine design : calculations using various log-probability distributions of heptane drops

A study of sprays formed by two impinging jets

Survey of the acoustic near field of three nozzles at a pressure ratio of 30

Survey of microstructures and mechanical properties of over-temperatured S-816 turbine buckets from J47 engines

Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds

Effects of string-support interference on the drag of an olgive-cylinder body with and without a boatail at 0.6 to 1.4 Mach number

Flight investigation of a roll-stabilized missile configuration at varying angles of attack at Mach numbers between 0.8 and 1.79

A flight investigation of area-suction and blowing boundary-layer control on the trailing-edge flaps of a 35 degree swept-wing-carrier-type airplane

Hydrodynamic characteristics over a range of speeds up to 80 feet per second of a rectangular modified flat plate having an aspect ratio of 0.25 and operating at several depths of submersion

Effects of free-stream Reynolds number, engine installation, and model scale on stability characteristics of a translating-spike inlet at Mach 2.0


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