TRAIL - Technical Report Archive and Image Library

Preliminary performance data for the J57-P-1 turbojet engine at altitudes up to 65,000 feet

A revised gust-load formula and a re-evaluation of v-g data taken on civil transport airplanes from 1933 to 1950

Rocket-model investigation of the longitudinal stability and drag characteristics of a 1/10-scale model of the Convair XF2Y-1 airplane having open ducts and the elevons deflected upward 3.5 degrees : TED No. NACA DE 375

Analytical and experimental studies of a divided-flow ram-jet combustor

Analysis of the turbojet for propulsion of supersonic bombers

Analytical determination of effect of turbine cooling-air-impeller performance on engine performance and comparison of experimentally determined performance of impellers with and without inducer vanes

Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio - transonic bumb method

Experimental heat-transfer and friction coefficients for air flowing through stacks of parallel flat plates

Experimental influence coefficients for the deflection of the wing of a full-scale, swept-wing bomber

Impingement of water droplets on wedges and double-wedge airfoils at supersonic speeds

Preliminary investigation of performance of variable-throat extended-plug-type nozzles over wide range of nozzle pressure ratios

An Investigation of the Hydrodynamic Characteristics of a 1/10-Size Powered Dynamic Model of the Martin M-267 Patrol-Type Seaplane with Two Forebody Configurations: TED No. NACA DE 376

Investigation of the Jet Effects on a Flat Surface Downstream of the Exit of a Simulated Turbojet Nacelle at a Free-Stream Mach Number of 2.02

Investigation of the NACA 4-(5)(05)-037 six- and eight-blade, dual-rotation propellers at positive and negative thrust at Mach numbers up to 0.90, including some aerodynamic characteristics of the NACA 4-(5)(05)-041 two- and four-blade, single-rotat

Effect of plug design on performance characteristics of convergent-plug exhaust nozzles

Effect of divergence angle on the internal performance characteristics of several conical convergent-divergent nozzles

Preliminary investigation of several target-type thrust-reversal devices

Investigation of noise field and velocity profiles of an afterburning engine

Effect of several jet-engine air-inlet configurations on the low-speed static longitudinal stability characteristics and quantity flow of a 1/6-scale model of the MX-1764 airplane

The effect of several jet-engine air-inlet configurations on the low-speed static lateral stability characteristics of a 1/6-scale model of the MX-1764 airplane

Effect of jet-nozzle-expansion ratio on drag of parabolic afterbodies

Design and experimental investigation of light-weight bases for air-cooled turbine rotor blades

Effects of secondary-air flow on annular base force of a supersonic airplane

Effects of rigid spoilers on the two-dimensional flutter derivatives of airfoils oscillating in pitch at high subsonic speeds

The aerodynamic characteristics at transonic speeds of a model with a 45 degree sweptback wing, including the effect of leading edge slats and a low horizontal tail

Analysis and construction of design charts for turbines with downstream stators

The application of a simplified lifting-surface theory to the prediction of the rolling effectiveness of plain spoiler ailerons at subsonic speeds

Application of several methods for determining transfer functions and frequency response of aircraft from flight data

An experimental investigation of hollow turbine blades for expandable jet engines

Axial-load fatigue properties of 24S-T and 75S-T aluminum alloy as determined in several laboratories

The effect of ground on the low-speed aerodynamics control, and control hinge-moment characteristics of a delta-wing-fuselage model with trailing-edge controls

Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics 3: effect of turbine stator adjustment

Comparison of experimental and theoretical normal-force distributions (including Reynolds number effects) on an ogive-cylinder body at Mach number 1.98

A wind-tunnel investigation of bomb release at a Mach number of 1.62

Force, moment, and pressure characteristics of several annular nose inlets at Mach number 3.85

Performance of a supersonic rotor having high mass flow

Investigation of an on-off inlet shock-position control on a 16-inch ram-jet engine

Investigation of thrust and drag characteristics of a plug-type exhaust nozzle

Thrust and drag characteristics of a convergent-divergent nozzle with various exhaust jet temperatures

High-altitude performance of 9.5-inch-diameter tubular experimental combustor with fuel staging

Investigation of effect of increased diffusion of rotor-blade suction-surface velocity on performance of transonic turbine

Performance of a 16-inch ram-jet engine with a can-type combustor at Mach numbers of 1.50 to 2.16

Theoretical performance characteristics of sharp-lip inlets at subsonic speeds

Wind-tunnel investigation at low speed of static and yawing characteristics of a 0.085-scale model of the Chance Vought XF8U-1 airplane: TED No. NACA DE 392

Wind-tunnel investigation at low speed of the yawing stability derivatives of a 1/10-scale model of the Douglas A4D-1 airplane: TED No. NACA DE 389

Wind-tunnel investigation at low speed of the rolling stability derivatives of a 1/10-scale model of the Douglas A4D-1 airplane: TED No. NACA DE 389

Comparison at supersonic speeds of translating spike inlets having blunt- and sharp-lip cowls

Investigation at supersonic speeds of a translating-spike inlet employing a steep-lip cowl

Thrust characteristics of a series of convergent-divergent exhaust nozzles at subsonic and supersonic flight speeds

Pumping and drag characteristics of an aircraft ejector at subsonic and supersonic speeds

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