Browse TRAIL Inventories

Effect of wing-tank location on the drag and trim of a swept-wing model as measured in flight at transonic speeds

Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections

Effects of inlet icing on performance of axial-flow turbojet engine in natural icing conditions

Effect of ram-jet pressure pulsations on supersonic-diffuser performance

Evaluation of a ducted-fan power plant designed for high output and good cruise fuel economy

Effect of Mach number on over-all performance of single-stage axial-flow compressor designed for high pressure ratio

Effects of molding conditions on some physical properties of glass-fabric unsaturated-polyester laminates

Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds

Experimental damping in pitch of 45 degree triangular wings

Experimental investigation of the effectiveness of various suction-slot arrangements as a means for increasing the maximum lift of the NACA 65(sub 3)-018 airfoil section

Experimental investigation of supersonic flow with detached shock waves for Mach numbers between 1.8 and 2.9

Internal film cooling experiments in 4-inch duct with gas temperatures to 2000 degrees F

Tabulated pressure coefficients and aerodynamic characteristics measured on the wing of the Bell X-1 airplane in pull-ups at Mach numbers from 0.53 to 0.99

Study of flow conditions and deflection angle at exit of two-dimensional cascade of turbine rotor blades at critical and supercritical pressure ratios

Study of compressor systems for a gas-generator engine

Summary report of results obtained during demonstration tests of the Northrop X-4 airplanes

An 8-foot axisymmetrical fixed nozzle for subsonic Mach numbers up to 0.99 and for a supersonic Mach number of 1.2

The effect of accelerating a hypothetical aircraft through the transonic range with controls fixed

Effect of air distribution on radial temperature distribution in one-sixth sector of annular turbojet combustor

Investigation of the pressure-ratio requirements of the Langley 11-inch hypersonic tunnel with a variable-geometry diffuser

Lift and pitching-moment interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02

Free-flight performance of 16-inch-diameter supersonic ram-jet units III : four units designed for combustion-chamber-inlet Mach number of 0.245 at free-stream Mach number of 1.8 (Units D-1, D-2, D-3, and D-4)

A transonic-wing investigation in the Langley 8-foot high-speed tunnel at high subsonic Mach numbers and at a Mach number of 1.2 : wing-fuselage configuration with a wing of 45 degrees sweepback, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfo

Turbojet-engine evaluation of AISI 321 and AISI 347 stainless steels as nozzle-blade materials

Tank investigation of the Grumman JRF-5 airplane fitted with hydro-skis suitable for operation on water, snow, and ice

Altitude performance and operational characteristics of 29-inch-diameter tail-pipe burner with several fuel systems and fuel-cooled stage-type flame holders on J35-A-5 turbojet engine

Altitude performance characteristics of tail-pipe burner with converging conical burner section on J47 turbojet engine

Altitude investigation of performance of turbine-propeller engine and its components

Altitude performance characteristics of turbojet-engine tail-pipe burner with variable-area exhaust nozzle using several fuel systems and flame holders

A theoretical investigation of the influence of auxiliary damping in pitch on the dynamic characteristics of a proportionally controlled supersonic canard missile configuration

Wing-tunnel investigation at Mach numbers from 0.50 to 1.29 of an all-movable triangular wing of aspect ratio 4 alone and with a body

Altitude-wind-tunnel investigation of combustion-chamber performance on J47 turbojet engine

Altitude-wind-tunnel investigation of operational characteristics of J47 turbojet engine

A theoretical investigation of the dynamic lateral oscillatory stability of an airplane having a 60 degree triangular wing

Low-speed lateral stability and aileron-effectiveness characteristics at a Reynolds number of 3.5 x 10(exp 6) of a wing with leading-edge sweepback decreasing from 45 degrees at the root to 20 degrees at the tip

The path and motion of scale models of jettisonable nose sections at supersonic speeds as determined from an investigation in the Langley free-flight apparatus

Model flight investigation of a nonlifting winged tow target

Stability characteristics at low speed of a 1/4-scale Bell X-5 airplane model with various modifications to the basic model configurations

Stability and control characteristics of a 1/4-scale Bell X-5 airplane model in the landing configuration

Preliminary investigation of porous walls as a means of reducing tunnel boundary effects at low-supersonic Mach numbers

Preliminary investigation of heat transfer to water flowing in an electrically heated Inconel tube

Pressure measurements at supersonic speeds on a section of a rectangular wing having an NACA 65-009 profile

Stability and control characteristics at low speed of a 1/4-scale Bell X-5 airplane model: Longitudinal stability and control

An analysis of the forces and pressure distribution on a wing with the leading edge swept back 37.25 degrees

Elevator-stabilizer effectiveness and trim of the X-1 airplane to a Mach number of 1.06

Effect of inlet temperature and humidity on thrust augmentation of turbojet engine by compressor-inlet injection

Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness of an elevon as a longitudinal control and the effects of camber and twist on the maximum lift-drag ratio at supersonic speeds

Numerical solution of equations for one-dimensional gas flow in rotating coolant passages

Temperature and pressure distributions in dual parallel jets impinging on the ground from a turbojet engine

Wing-flow measurements of longitudinal stability and control characteristics of a canard airplane configuration with a 45 degree sweptback wing and a triangular all-movable control surface


Published Year

Subject

Author

‹‹ previous 1 2 ... 140 141 142 143 144 145 146 ... 280 281 next ››