Browse TRAIL Inventories

Performance of mixed-flow impeller, model MFI-1B, with diffuser vanes at equivalent impeller speeds from 1100 to 1700 feet per second

Performance of five low-temperature-ratio ram-jet combustors over range of simulated altitudes

Tests in the Ames 40- by 80-foot wind tunnel of the effects of varying wing modifications on the longitudinal characteristics of two-triangular wing airplane models with and without horizontal tails

Matrix methods for determining the longitudinal-stability derivatives of an airplane from transient flight data

Jet effects on pressure loading of all-movable horizontal stabilizer

Wind pressure distributions at low lift for the XF-92A delta-wing airplane at transonic speeds

Preliminary investigation of a technique for stability studies of a self-propelled model of a submerged submarine

Preliminary investigation of an asymmetric swept nose inlet of circular projection at Mach number 3.85

A preliminary study of the preparation of slurry fuels from vaporized magnesium

Preliminary wind tunnel investigation of two types of jet-exit configurations for control of aircraft

Preliminary investigation at subsonic and transonic speeds of the aerodynamic characteristics of a biplane composed of a sweptback and a sweptforward wing joined at the tips

Preliminary drag measurements of the consolidated Vultee XF-92A delta-wing airplane in flight tests to a Mach number of 1.01

Lift and drag characteristics of the Douglas X-3 research airplane obtained during demonstration flights to a Mach number of 1.20

Lateral control characteristics of two structural similar flexible wings with 45 degrees sweep: a sweptback wing and a wing with M plan form

Lift and drag characteristics of the Douglas D-558-II research airplane obtained in exploratory flights to a Mach number of 2.0

Longitudinal aerodynamic characteristics to large angles of attack of a cruciform missile configuration at a Mach number of 2

A low-speed investigation of the aerodynamic, control, and hinge-moment characteristics of two types of controls and balancing tabs on a large-scale thin delta-wing-fuselage model

Measurement of heat-transfer and friction coefficients for flow of air in noncircular ducts at high surface temperatures

Measurements of normal-force-coefficient fluctuation on four 9-percent-thick airfoils having different locations of maximum thickness

Effect of ignitor design and ignitor spark-gap environment on ignition in a turbojet combustor

Ignition of ammonia and mixed oxides of nitrogen in 200-pound-thrust rocket engines at 160 F

Comparison of Experimental Hydrodynamic Impact Loads and Motions for a V-Step and a Transverse-Step Hydro-Ski

On traveling waves in beams

Comparison of normal load factors experienced with jet fighter airplanes during combat operations with those of flight tests conducted by the NACA during operational training

Effect of channel geometry on the quenching of laminar flames

A study of the use of controls and the resulting airplane response during service training operations of four jet fighter airplanes

Correlation of isothermal contours formed by penetration of jet of liquid ammonia directed normal to an airstream

Drag data for 16-inch-diameter ram-jet engine with double-cone inlet in free flight at Mach numbers from 0.7 to 1.8

Design and test of mixed-flow impellers 4: experimental results for impeller models MF-1 and MF-2 with changes in blade height

Effect of nozzle contour on drag of parabolic afterbodies

Aerodynamic characteristics of several tip controls on a 60 degree wing at a Mach number of 1.61

Aerodynamic characteristics of two flat-bottomed bodies at Mach number of 3.12

Analytical study of losses at off-design conditions for a fixed geometry turbine

Angle-of-attack-supersonic performance of a configuration consisting of a ramp-type scoop inlet located either on top or bottom of a body of revolution

Analytical investigation of off-design performance of a transonic turbine

The aerodynamic characteristics of two series of lifting bodies at Mach number 6.86

Buffeting forces on two-dimensional airfoils as affected by thickness and thickness distribution

Comparison of experimental with calculated results for the lifting effectiveness of a flexible 45 degree sweptback wing of aspect ratio 6.0 at Mach numbers from 0.8 to 1.3

Comparison of effects of ailerons and combinations of spoiler-slot-deflector arrangements on spin recovery of sweptback-wing model having mass distributed along the fuselage

Analysis of performance of four symmetrical-diagram-type subsonic inlet-stage axial-flow compressors

Aerodynamic characteristics of several flap-type trailing-edge controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01

A comparison of flight measurements with calculations of the horizontal-tail root bending moments for a jet-powered bomber airplane

Comparison of low-speed rotor and cascade performance for medium-camber NACA 65-(C(sub lo)A(sub 10) 10 compressor-blade sections over a wide range of rotor blade-setting angles at solidities. of 1.0 and 0.5

Analysis of off-design operation of high Mach number supersonic turbojet engines

Characteristics of a hydraulic control determined from transient data obtained with a turbojet engine at altitude

Characteristics of flow about axially symmetric isentropic spikes for nose inlets at Mach number 3.85

Combined compressor coolant injection and afterburning for turbojet thrust augmentation

Combustion performance of two experimental turbojet annular combustors at conditions simulating high-altitude supersonic flight

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines II : analytical techniques

Blow-out velocities of various petroleum, slurry, and hydride fuels in a 1 7/8-inch diameter combustor


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