TRAIL - Technical Report Archive and Image Library

Free-spinning tunnel investigation of the 1/21-scale model of the Chance Vought F7U-3 airplane: TED No. NACA DE 362

Optical methods involving light scattering for measuring size and concentration of condensation particles in supercooled hypersonic flow

Correlation of analog solutions with experimental sea-level transient data for controlled turbine-propeller engine, including analog results at altitudes

Analytical investigation of flow through high-speed mixed-flow turbine

Aerodynamic characteristics of a slender cone-cylinder body of revolution at a Mach number of 3.85

Characteristics of a transonic test section with various slot shapes in the Langley 8-foot high-speed tunnel

Compressive strength of flanges

An analysis of base pressure at supersonic velocities and comparison with experiment

Evaluation of the reduced-mass method of representing wing-lift effects in free-fall drop tests of landing gears

System analyses and autopilot design for automatic roll stabilization of a supersonic pilotless aircraft

A simplified instrument for recording and indicating frequency and intensity of icing conditions encountered in flight

A study of effects of viscosity on flow over slender inclined bodies of revolution

A small-deflection theory for curved sandwich plates

The static longitudinal characteristics at Mach numbers up to 0.95 of a triangular-wing canard model having a triangular control

Summary of Methods for Calculating Dynamic Lateral Stability and Response and for Estimating Lateral Stability Derivatives

Summary of results obtained by transonic-bump method on effects of plan form and thickness on lift and drag characteristics of wings at transonic speeds

Hydrodynamic investigation of a 1/13-scale model of the consolidated vultee skate 7 seaplane equipped with twin hydro-skis : TED No. NACA DE 342

Effects of horizontal-tail position, area, and aspect ratio on low-speed static longitudinal stability and control characteristics of a 60 degrees triangular-wing model having various triangular-all-movable horizontal tails

Investigation at zero angle of attack of a 16-inch ram jet engine in 8- by 6-foot supersonic wind tunnel

Investigation of altitude ignition, acceleration and steady-state operation with single combustor of J47 turbojet engine

Altitude-performance and Reynolds number investigation of centrifugal-flow-compressor turbojet engine

Altitude-ignition limit of a turbojet engine using a condenser-discharge ignition system

Wire cloth as porous material for transpiration-cooled walls

A wind-tunnel investigation of the aerodynamic characteristics of a full-scale sweptback propeller and two related straight propellers

Wind-tunnel investigation of the aerodynamic characteristics of a 1/15-scale model of the Northrop MX-775A missile

Two-dimensional cascade investigation of the maximum exit tangential velocity component and other flow conditions at the exit of several turbine blade designs at supercritical pressure ratios

A two-dimensional cascade study of the aerodynamic characteristics of a turbine-rotor blade suitable for air cooling

Theoretical study of some methods for increasing the smoothness of flight through rough air

Low-speed wind-tunnel investigation of lateral control characteristics of a 60 degrees triangular-wing model having half-delta tip controls

A self-synchronizing stroboscopic Schlieren system for the study of unsteady air flows

Synthesis of cyclopropane hydrocarbons from methylcyclopropyl ketone 3: 2-cyclopropyl-1-butene, cis and trans 2-cyclopropyl-2-butene, and 2-cyclopropylbutane

Synthesis, purification and physical properties of hydrocarbons of the naphthalene series 1: 1-methylnaphthalene, 1-ethylnaphthalene, 1-butylnaphthalene, and 1-isobutylnaphthalene

An improved approximate method for calculating lift distributions due to twist

Experimental study of an angle-of-attack vane mounted ahead of the nose of an airplane for use as a sensing device for an acceleration alleviator

Flight investigation of some factors affecting the critical tail loads on large airplanes

Flight investigation of the effect of transient wing response on wing strains of a twin-engine transport airplane in rough air

General plastic behavior and approximate solutions of rotating disk in strain-hardening range

An investigation of aircraft heaters XXXVIII : determination of thermal performance of rectangular- and trapezoidal-shaped inner-skin passages for anti-icing systems

The Indicial Lift and Pitching Moment for a Sinking or Pitching Two-Dimensional Wing Flying at Subsonic or Supersonic Speeds

Inelastic column behavior

Theoretical characteristics of two-dimensional supersonic control surfaces

Theoretical force and moments due to sideslip of a number of vertical tail configurations at supersonic speeds

Two axial-symmetry solutions for incompressible flow through a centrifugal compressor with and without inducer vanes

Unsteady laminar boundary-layer flow

The use of an uncalibrated cone for determination of flow angles and Mach numbers at supersonic speeds

Linearized solution and general plastic behavior of thin plate with circular hole in strain-hardening range

Method of matching components and predicting performance of turbine-propeller engine

A method of solving the direct and inverse problem of supersonic flow along arbitrary stream filaments of revolution in turbomachines

Rupture properties of low carbon N-155 type alloys made with a columbium-tantalum ferro-alloy

Stability and control characteristics of a complete airplane model having a wing with quarter-chord line swept back 40 degrees, aspect ratio 2.50, and taper ratio 0.42

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