Browse TRAIL Inventories

Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3.4 with circular-arc airfoil sections at Reynolds numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6)

Design and performance of experimental axial-discharge mixed-flow compressor I : impeller design theory

Inlet Icing and Effectiveness of Hot-Gas Bleedback for Ice Protection of Turbojet Engine

Application of one part of Von Karman's two-dimensional transonic similarity law to drag data of NACA 65-series wings

Axial fatigue tests at zero mean stress of 24S-T and 75S-T aluminum-alloy strips with a central circular hole

Wind-tunnel investigation of horizontal tails 3: unswept and 35 degrees swept-back plan forms of aspect ratio 6

Investigation of wing characteristics at a Mach number of 1.53 3: unswept wings of differing aspect ratio and taper ratio

Investigation of wing characteristics at a Mach number of 1.53 2: swept wings of taper ratio 0.5

Calculation of the aerodynamic loading of swept and unswept flexible wings of arbitrary stiffness

Ram-recovery characteristics of NACA submerged inlets at high subsonic speeds

Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers 1: shock diffuser with triple-shock projecting cone

An exploratory investigation of the relative merits of split and chord-extension flaps on a 45 degrees swept-back wing

Investigation of effects of movable exhaust-nozzle plug on operational performance of 20-inch ram jet

Ditching tests of a 1/15-scale model of the Fairchild C-82 airplane

An investigation at low speed of a 51.3 degrees sweptback semispan wing with a raked tip and with 16.7-percent-chord ailerons having three spans and three trailing-edge angles

An investigation at low speed of a 51.3 degree sweptback semispan wing equipped with 16.7-percent-chord plain flaps and ailerons having various spans and three trailing-edge angles

Gas-turbine-engine operation with variable-area fuel nozzles

Ice protection of turbojet engines by inertia separation of water I : alternate-duct system

Ice protection of turbojet engines by inertia separation of water III : annular submerged inlets

Ice protection of turbojet engines by inertia separation of water II : single-offset-duct system

A limit pressure coefficient and an estimation of limit forces on airfoils at supersonic speeds

Determination of average heat-transfer coefficients for a cascade of symmetrical impulse turbine blades 1: heat transfer from blades to cold air

Design and performance of experimental axial-discharge mixed-flow compressor II : performance of impeller

Aerodynamic characteristics of a two-blade NACA 10-(3)(12)-03 propeller

Analysis of parameters for thrust control of a turbojet engine equipped with air-inlet throttle and variable-area exhaust nozzle

Aerodynamic characteristics of a two-blade NACA 10-(3)(08)-03R propeller

The effect of negative dihedral, tip droop, and wing-tip shape on the low-speed aerodynamic characteristics of a complete model having a 45 degrees sweptback wing

Evaluation of gust and draft velocities from flights of F-61C airplanes within thunderstorms August 21, 1947 to August 25, 1947 at Clinton County Army Air Field, Ohio

Evaluation of gust and draft velocities from flights of P-61C airplanes within thunderstorms July 31, 1947 to August 6, 1947 at Clinton County Army Air Field, Ohio

Evaluation of gust and draft velocities from flights of an AT-6 airplane within cumulus clouds July 1, 1947 to July 22, 1947 at Clinton County Army Air Field, Ohio

Experimental data concerning the effect of high heat-input rates on the pressure drop through radiator tubes

Aerodynamic characteristics at subsonic and supersonic Mach numbers of a thin triangular wing of aspect ratio 2 II : maximum thickness at midchord

Static longitudinal aerodynamic characteristics of a 52 degree sweptback wing of aspect ratio 2.88 at Reynolds numbers from 2,000,000 to 11,000,000

Study of stress states in gas-turbine disk as determined from measured operating-temperature distributions

Tests of a triangular wing of aspect ratio 2 in the Ames 12-foot pressure wind tunnel III : the effectiveness and hinge moments of a skewed wing-tip flap

Tests of a triangular wing of aspect ratio 2 in the Ames 12-foot pressure wind tunnel II : the effectiveness and hinge moments of a constant-chord plain flap

Effect of a nacelle on the low-speed aerodynamic characteristics of a swept-back wing

Investigation at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees swept airfoil of biconvex section at several angles of attack

Investigation at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees swept airfoil of biconvex section at zero lift

Tank spray tests of a jet-powered model fitted with NACA hydro-skis

Tests of the NACA 64(sub 1)-012 and 64(sub 1)A012 airfoils at high subsonic Mach numbers

Aerodynamic characteristics at high speeds of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller

Aerodynamic characteristics at high speeds of full-scale propellers having Clark Y blade sections

Low-speed pressure distributions over the drooped-nose flap of a 42 degrees sweptback wing with circular-arc airfoil sections at a Reynolds number of 5.3 x 10(exp 6)

Shear lag in axially loaded panels

A study of skin temperatures of conical bodies in supersonic flight

Effects of surface finish, of certain defects, and of repair of defects by welding on fatigue strength of 355-T6 sand-castings and effects of prior fatigue stressing on tensile properties

Dynamometer-stand investigation of the muffler used in the demonstration of light-airplane noise reduction

Effects of fuel-nozzle carbon deposition on combustion efficiency of single tubular-type, reverse-flow turbojet combustor at simulated altitude conditions

A general small-deflection theory for flat sandwich plates


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