TRAIL - Technical Report Archive and Image Library

An investigation at high subsonic speeds of the pressure distributions on a 45 degree sweptback vertical tail in sideslip with and without a 45 degree sweptback horizontal tail located on the fuselage center line

Investigation of compressible flow mixing losses obtained downstream of a blade row

Investigation at high subsonic speeds of the effect of adding various combinations of missiles on the aerodynamic characteristics of sweptback and unswept wings combined with a fuselage

Investigation at high subsonic speeds of the pressure distributions on a 45 degree sweptback horizontal tail mounted at 50-percent and 100-percent vertical-tail span

Effects of additives on corrosion and mass transfer in sodium hydroxide - nickel systems under free-convection conditions

Dynamic corrosion of nickel at 1500 F by sodium hydroxide with various additives in a torrid circulating apparatus

Dynamic corrosion in an iron - stainless steel toroid by sodium at 900 F

Investigation of effect of number and width of annular flame-holder gutter on afterburner performance

Explosion and combustion properties of alkylsilanes I : temperature-composition limits of explosion for methyl-,dimethyl-,trimethyl-,tetramethyl-,and vinylsilane at atmospheric pressure

Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth

Ground tests of the elevator power control system and feel device in a Boeing B-47A airplane

Effects of angle of attack and airfoil profile on the two-dimensional flutter derivatives for airfoils oscillating in pitch at high subsonic speeds

Effects of airfoil profile on the two-dimensional flutter derivatives for wings oscillating in pitch at high subsonic speeds

Chordwise pressures and section moment force and moment coefficients at high subsonic speeds near midspan of a tapered 35 degree sweptback wing with a flap-type control and an attached tab

The effect of lip shape on a nose-inlet installation at Mach numbers from 0 to 1.5 and a method for optimizing engine-inlet combinations

Free-flight investigation of the full-scale Hughes Falcon missile, D configuration, to determine aileron effectiveness and damping in roll

Free-flight tests of 45 degree swept wings of aspect ratio 3.15 and taper ratio 0.54 to measure wing damping of the first bending mode and to investigate the possibility of flutter at transonic speeds

Effect of nose shape and trailing-edge bluntness on the aerodynamic characteristics of an unswept wing of aspect ratio 3.1, taper ratio 0.4, and 3-percent thickness

Effect of a leading-edge flap upon the lift, drag, and pitching moment of an airplane employing a thin, unswept wing

Effects of diffuser and center-body length on performance of annular diffusers with constant-diameter outer walls and with vortex-generator flow controls

Analysis of rocket, ram-jet, and turbojet engines for supersonic propulsion of long-range missiles 1: rocket-engine performance

Effects of base bleed on the base pressure of blunt-trailing-edge airfoils at supersonic speeds

Free-flight zero-lift drag-rise measurements of equivalent bodies of revolution of several versions of the Douglas XF4D-1 airplane at transonic speeds: TED No. NACA AD 394

Experimental investigation of drag of afterbodies with exiting jet at high subsonic Mach numbers

Cascade investigation of a related series of 6-percent-thick guide-vane profiles and design charts

Drag and longitudinal trim characteristics of a low-tail version of the North American YF-100A airplane as determined from the flight test at low lift of a 0.11-scale rocket-powered model at Mach numbers between 0.75 and 1.78

Minimum drag of 0.11-scale rocket-powered models of the Chance Vought XF8U-1 airplane, with and without nose modifications, at Mach numbers between 0.85 and 1.30 : TED No. NACA DE 392

A summary of the drag and longitudinal trim at low lift of the North American YF-100A airplane at Mach numbers from 0.75 to 1.77 as determined by flight tests of 0.11-scale rocket models

Altitude investigation of 20-inch-diameter ram-jet engine with annular-piloted combustor

Performance of a vaporizing annular turbojet combustor at simulated high altitudes

Preliminary investigation of an annular turbojet combustor having a catalytic-coated liner

A comparison of the longitudinal aerodynamic characteristics at Mach numbers up to 0.94 of swept back wings having NACA 4-digit or NACA 64A thickness distributions

Summary of some rocket-model investigations of effects of wing aspect ratio and thickness on aileron rolling effectiveness including some effects of spanwise aileron location for sweptback wings with aspect ratio of 8

Some effects of aileron span, aileron chord, and wing twist on rolling effectiveness as determined by rocket-powered model tests and theoretical estimates

Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data

Tests of the Northrop XB-62 Missile in the Ames 40- by 80-Foot Wind Tunnel

Longitudinal Aerodynamic Characteristics to Large Angles of Attack of a Cruciform Missile Configuration at a Mach Number of 2

Preliminary Investigation of a Technique for Stability Studies of a Self-Propelled Model of a Submerged Submarine

The Resistance to Air Flow of Porous Materials Suitable for Boundary-Layer-Control Applications Using Area Suction

The Small-Disturbance Method for Flow of a Compressible Fluid With Velocity Potential and Stream Function as Independent Variables

Lift and Moment Equations for Oscillating Airfoils in an Infinite Unstaggered Cascade

Measurement of Heat Transfer in the Turbulent Boundary Layer on a Flat Plate in a Supersonic Flow and Comparison With Skin-Friction Results

Results of Edge-Compression on Stiffened Flat-Sheet Panels of Alclad and Nonclad 14S-T6, 24S-T3, and 75S-T6 Aluminum Alloys

Application of Two-Dimensional Vortex Theory to the Prediction of Flow Fields Behind Wings of Wing Body Combinations at Subsonic and Supersonic Speeds

Statistical Study of Overstressing in Steel

Tests of Bonded and Riveted Sheet-Stringer Panels

Span Load Distribution Resulting From Constant Vertical Acceleration for Thin Sweptback Tapered Wings With Streamwise Tips: Supersonic Leading and Trailing Edges

Use of a Hot-Wire Anemometer in Shock-Tube Investigations

Ion Tracer Technique for Airspeed Measurement at Low Densities

A Method for Estimating the Effect of Turbulent Velocity Fluctuations in the Boundary Layer on Diffuser Total-Pressure-Loss Measurements

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