Browse TRAIL Inventories

The effect of rate of change of angle of attack on the maximum lift of a small model

Estimation of the damping in roll of supersonic-leading-edge wing-body combinations

Experimental investigation of stiffened circular cylinders subjected to combined torsion and compression

Experimental investigation of the effect of vertical-tail size and length of fuselage shape and length on the static lateral stability characteristics of a model with 45 degree sweptback wing and tail surfaces

Experiments in external noise reduction of light airplanes

Tables of wing-aileron coefficients of oscillating air forces for two-dimensional supersonic flow

Statistical explanation of spontaneous freezing of water droplets

Supersonic flow around circular cones at angles of attack

Resistance of six cast high-temperature alloys to cracking caused by thermal shock

Study of effects of sweep on the flutter of cantilever wings

A small-deflection theory for curved sandwich plates

Sound measurements for five shrouded propellers at static conditions

Spanwise loading for wings and control surfaces of low aspect ratio

Static longitudinal stability and control of a convertible-type airplane as affected by articulated-and rigid-propeller operation

Propeller flight investigation to determine the effects of blade loading

Synthesis and purification of alkyldiphenylmethane hydrocarbons 1: 2-methyldiphenylmethane, 3-methyldiphenylmethane, 2-ethyldiphenylmethane, 4-ethyldiphenylmethane and 4-isopropyldiphenylmethane

Dynamic similitude between a model and a full-scale body for model investigation at full-scale Mach number

Dynamics of a turbojet engine considered as a quasi-static system

Improvement of high-temperature properties of magnesium-cerium forging alloys

Investigation of 75-millimeter-bore cylindrical roller bearings at high speeds 2: lubrication studies - effect of oil-inlet location, angle, and velocity for single-jet lubrication

An investigation of aircraft heaters XXXIII : experimental determination of thermal and hydrodynamical behavior of air flowing along finned plates

Investigation of 75-millimeter-bore cylindrical roller bearings at high speeds: 1: Initial studies

Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars

Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tipssupersonic leading edges

Theoretical effect of inlet hub-tip-radius ratio and design specific mass flow on design performance of axial-flow compressors

Turbojet thrust augmentation by evaporation of water prior to mechanical compression as determined by use of psychrometric chart

Theoretical investigation and application of transonic similarity law for two dimensional flow

Theory of helicopter damping in pitch or roll and a comparison with flight measurements

Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper: Mach lines behind flap leading and trailing edges

Theoretical wave drags and pressure distributions for axially symmetric open-nose bodies

Time-dependent downwash at the tail and the pitching moment due to normal acceleration at supersonic speeds

Low-speed investigation of the stalling of a thin, faired, double-wedge airfoil with nose flap

A method of determining the effect of airplane stability on the gust load factor

Method of experimentally determining radial distributions of velocity through axial-flow compressor

Effect of heat and power extraction on turbojet-engine performance 1: analytical method of performance evaluation with compressor-outlet air bleed

Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces

Effect of heat and power extraction on turbojet-engine performance 2: effect of compressor-outlet air bleed for specific modes of engine operation

Effect of heat and power extraction on turbojet-engine performance 3: analytical determination of effects of shaft-power extraction

Formulas for source, doublet, and vortex distributions in supersonic wing theory

Chart for simplifying calculations of pressure drop of a high-speed compressible fluid under simultaneous action of friction and heat transfer - application to combustion-chamber cooling passages

The interpretation of biaxial-tension experiments involving constant stress ratios

An experimental investigation of the NACA 631-012 airfoil section with leading-edge and midchord suction slots

An analysis of the normal accelerations and airspeeds of a four-engine airplane type in postwar commercial transport operations on trans-Pacific and Caribbean-South American routes

An approximate method of calculating pressures in the tip region of a rectangular wing of circular-arc section at supersonic speeds

Approximate aerodynamic influence coefficients for wings of arbitrary plan form in subsonic flow

Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds : supersonic leading and trailing edges

The effects of stability of spin-recovery tail parachutes on the behavior of airplanes in gliding flight and in spins

Frequency response of positive-displacement variable stroke fuel pump

Investigation of the flow through a single-stage two-dimensional nozzle in the Langley 11-inch hypersonic tunnel

Critical stress of plate columns


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