Browse TRAIL Inventories

Effect of Variable Viscosity and Thermal Conductivity on High-Speed Slip Flow Between Concentric Cylinders

Recovery corrections for butt-welded, straight-wire thermocouples in high-velocity, high-temperature gas streams

Statistical survey of icing data measured on scheduled airline flights over the United States and Canada from November 1951 to June 1952

Experimental investigation of external water-spray cooling in a turbojet engine utilizing several injection configurations including orifices in the rotor-blade bases

Application of oblique-shock sensing system to ram-jet-engine flight Mach number control

Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine

A survey of methods for turbojet thrust measurement applicable to flight installation

Combustion of aluminum borohydride in a supersonic wind tunnel

Correlation of turbojet combustor carbon formation with smoke-volatility index, smoke point, and NACA K factor

Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles

Average bond energies between boron and elements of the fourth, fifth, sixth, and seventh groups of the periodic table

Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60©� delta wing at Mach numbers from 0.75 to 1.96

Characteristics of loads in rough air at transonic speeds of rocket-powered models of a canard and a conventional-tail configuration

An aerodynamic and hydrodynamic investigation of two multi-jet water-based aircraft having low transonic drag rise

Loads associated with spoilers at supersonic speeds

Loads on wings due to spoilers at subsonic and transonic speeds

Vertical and drag ground-reaction forces developed in landing impacts of a large airplane

A free-flight investigation at high subsonic and low supersonic speeds of the rolling effectiveness and drag of three spoiler controls having potentially low actuating-force requirements

The rolling moment due to sideslip of swept wings at subsonic and transonic speeds

Analysis of aerodynamic blade-loading-limit parameters for NACA 65-(C[sub zeta]₀A₁₀) 10 compressor-blade sections at low speeds

An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds

Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5

Effect of surface roughness on characteristics of spherical shock waves

Some observations on loss of static strength due to fatigue cracks

Preliminary investigation of the failure of pressurized stiffened cylinders

Summary of recent theoretical and experimental work on box-beam vibrations

Preliminary investigation of the compressive strength and creep lifetime of 2024-T3 (formerly 24S-T3) aluminum-alloy plates at elevated temperatures

Tensile properties of some sheet materials under rapid-heating conditions

A study of the response of panels to random acoustic excitation

A free-flight investigation of the effects of simulated sonic turbojet exhaust on the drag of a boattail body with various jet sizes from Mach number 0.87 to 1.50

Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration

Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region

Calculated effects of the lateral acceleration derivatives on the dynamic lateral stability of a delta-wing airplane

A low-speed investigation of a thin 60©� delta wing equipped with a double slotted flap to determine the chordwise pressure distribution and the effect of vane size

Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems

Transonic Zero-Lift Drag Tests of Four Equivalent-Body-of-Revolution Models Representing Variations of the Convair F-102 Airplane

Free-Spinning and Recovery Characteristics of a 1/18-Scale Model of the Ryan X-13 Airplane as Determined from Tests in the Langley 20-Foot Free-Spinning Tunnel

Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102A Airplane at Transonic Speeds

Turbojet Propulsion-System Research and the Resulting Effects on Airplane Performance

Emergency Spin-Recovery Device for the 1/18-Scale Model of the Ryan X-13 Airplane as Determined from Tests in the Langley 20-Foot Free-Spinning Tunnel

Aerodynamic Design of Axial-Flow Compressors. VII - Blade-Element Flow in Annular Cascades

Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8

Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination

A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body

Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of an aileron located at two spanwise positions

Loads on thin wings at transonic speeds

A study of means for rationalizing airplane design loads

Landing conditions for large airplanes in routine operations

Some factors affecting the variation of pitching moment with sideslip of aircraft configurations

Investigation at transonic speeds of the hinge-moment characteristics of a 1/8-scale model of the X-1E aileron


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