Browse TRAIL Inventories

Effect of oxygen concentration of the inlet oxygen-nitrogen mixture on the combustion efficiency of a single J33 turbojet combustor

Aerodynamic characteristics of two 25-percent-area trailing-edge flaps on an aspect ratio 2 triangular wing at subsonic and supersonic speeds

An analytical method for evaluating factors affecting application of transpiration cooling to gas turbine blades

An analytical study of the comparative performance of four air-induction systems for turbojet-powered airplanes designed to operate at Mach numbers up to 1.5

Analytical study of static and low-speed performance of thin propellers using two-speed gear ratios to obtain optimum rotational speeds

Comparison of calculated and experimental temperatures of water-cooled turbine blades

Combustion efficiency of homogeneous fuel-air mixtures in a 5-inch ram-jet-type combustor

Analysis of stage matching and off-design performance of multistage axial-flow compressors

The aerodynamic characteristics of a supersonic aircraft configuration with a 40 degree sweptback wing through a Mach number range from 0 to 2.4 obtained from various sources

Aerodynamic characteristics of two-plane, unswept tapered wings of aspect ratio 3 and 3-percent thickness from tests on a transonic bump

Characteristics of flap-type spoiler ailerons at various locations on a 60 degree delta wing with a double slotted flap

Characteristics of swept wings at high speeds

Combustion efficiency performance of a MIL-F-5624 type fuel and monomethylnapthalene in a single vaporizing combustor

Component and over-all performance evaluation of an axial-flow turbojet engine over a range of engine-inlet Reynolds numbers

Analysis of coolant-flow requirements for an improved, internal-strut-supported, air-cooled turbine-rotor blade

An analysis of axial- and centrifugal-flow turbojet-engine performance with variable-area exhaust nozzle

Analysis of a Nuclear-Powered Liquid-Metal Ducted-Fan Cycle

Analysis of a liquid-metal turbine-propeller cycle for propulsion of low-speed nuclear-powered aircraft

Bodies of Revolution for Minimum Drag at High Supersonic Airspeeds

Effect of trailing edge thickness on lift at supersonic velocities

Effect of water vapor on combustion of magnesium hydrocarbon slurry fuels in small-scale afterburner

The effect of various aerodynamic balances on the low-speed lateral-control and hinge-moment characteristics of a 0.20-chord partial-span outboard aileron on a wing with leading edge swept back 51.3 degrees

The effective downwash characteristics at transonic speeds of a 6-percent-thick wing with 47 degrees of sweepback in combination with a cylindrical body as determined from force measurements of a horizontal tail

Effects of internal configuration on afterburner shell temperatures

Effect of fuel properties on carbon deposition in atomizing and prevaporizing turbojet combustors

The effects of tip-mounted jet nacelles on the transonic characteristics of low-aspect-ratio wings

Effects of three types of blunt trailing edges on the aerodynamic characteristics of a plane tapered wing of aspect ratio 3.1, with a 3-percent- thick biconvex section

The effects of sweepback on longitudinal characteristics of a 1/30-scale semispan model of the Bell X-5 airplane as determined from NACA wing-flow tests at transonic speeds

Effects of twist and camber, fences, and horizontal-tail height on the low-speed longitudinal stability characteristics of a wing-fuselage combination with a 45 degree sweptback wing of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)

Experimental and theoretical study of factors influencing the longitudinal stability of an air-to-air missile at a Mach number of 1.4

Experimental investigation of boundary-layer suction through slots to obtain extensive laminar boundary layers on a 15-percent-thick airfoil section at high Reynolds numbers

An experimental cascade study of the effects of a solidity reduction on the two-dimensional aerodynamic characteristics of a turbine-rotor blade suitable for air cooling

Experimental investigation of flow in an annular cascade of turbine nozzle blades of constant discharge angle

Experimental investigation of the effect of forebody bluntness on the pressure recovery and drag of a twin-scoop inlet-body combination at Mach numbers of 1.4 and 1.7

An experimental investigation of the combustion properties of a hydrocarbon fuel and several magnesium and boron slurries

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effect at M = 2.01 of nacelle shape and position on the aerodynamic characteristics in

Aerodynamic characteristics at transonic speeds of a wing having a 45 degree sweep, aspect ratio 8, taper ratio 0.45, and airfoil sections varying from the NACA 63A010 section at the root to the NACA 63A006 section at the tip.

Aerodynamic characteristics extended to high angles of attack at transonic speeds of a small-scale 0 degree sweep wing, 45 degree sweptback wing, and 60 degree delta wing

Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch

Aerodynamic characteristics at transonic speeds of a 60 degree delta wing equipped with a constant-chord flap-type control with and without an unshielded horn balance : transonic-bump method

The aerodynamic characteristics at transonic speeds of an all-movable, tapered, 45 degrees sweptback, aspect-ratio-4 tail surface deflected about a skewed hinge axis

Some observations of flow at the throat of a two-dimensional diffuser at a Mach number of 3.85

Skin-friction drag and boundary-layer transition on a parabolic body of revolution (NACA RM-10)at a Mach number of 1.6 in the Langley 4-by-4 foot supersonic pressure tunnel

A small-scale investigation of the effect of spanwise and chordwise positioning of an ogive-cylinder underwing nacelle on the high-speed aerodynamic characteristics of a 45 degree sweptback tapered-in-thickness wing of aspect ratio 6

Some factors affecting fabrication and high-temperature strength of molybdenum disilicide

Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment

Some stress rupture and creep properties of molybdenum disilicide in the range of 1600 to 2000 F

Results of flight tests to determine the drag of finite-length cylinders at high Reynolds numbers for a Mach number range of 0.5 to 1.3

Survey of some preliminary investigations of supersonic diffusers at high Mach numbers

Tests of a centering spring used as an artificial feel device on the elevator of a fighter airplane


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