TRAIL - Technical Report Archive and Image Library

Theoretical prediction of the side force on stores attached to configurations traveling at supersonic speeds

Wind-tunnel investigation of the static longitudinal and lateral stability of a 1/62-scale model of the X-1E at supersonic speeds

Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule

A flight and analytical study of methods for reducing automatic-interceptor tracking errors caused by target maneuvers

Flight and analytical study of roll requirements of a fighter airplane

Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds

An Experimental Investigation of Sting-Support Effects on Drag and a Comparison with Jet Effects at Transonic Speeds

Lift, Drag, Static Stability, and Buffet Boundaries of a Model of the McDonnell F3H-1N Airplane at Mach Numbers from 0.40 to 1.27, TED No. NACA DE 351

Longitudinal and Lateral Stability, Control Characteristics, and Vertical-Tail-Load Measurements for 0.03-Scale Model of the Avro CF-105 Airplane at Mach Number 1.41

Concluding Report on Free-Spinning and Recovery Characteristics of a 1/24-Scale Model of the Grumman F11F-1 Airplane, TED No. NACA AD 395

Ditching Investigation of a 1/12-Scale Model of the Douglas F4D-1 Airplane, TED No. NACA DE 384

Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches

An investigation of the hydrodynamic characteristics of a dynamic model of a transonic seaplane design having a planing-tail hull

Low-speed static stability characteristics of a cambered-delta-wing model

Lift-curve slopes determined in flight on a flexible swept-wing jet bomber

Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections

The Interference Effects of a Body on the Spanwise Load Distributions of Two 45 Degree Sweptback Wings of Aspect Ratio 8.02 from Low-Speed Tests

Operation of an experimental air-cooled turbojet engine at turbine-inlet temperatures from 2200 R to 2935 R

Impingement of Droplets in 60 Degree Elbows with Potential Flow

An Analysis of Air-turborocket Engine Performance Including Effects of Component Changes

Summary of NACA Research on Afterburners for Turbojet Engines

Turbojet Performance and Operation at High Altitudes With Hydrogen and JP-4 Fuels

Performance characteristics of an underslung vertical-wedge inlet with porous suction at Mach numbers of 0.63 and 1.5 to 2.0

Performance of a Blunt-lip Side Inlet With Ramp Bleed, Bypass, and a Long Constant-area Duct Ahead of the Engine- Mach Numbers 0.66 and 1.5 to 2.1

Investigation of heat transfer from a stationary and rotating ellipsoidal forebody of fineness ratio 3

Analysis of turbojet and ram-jet engine cycles using various fuels

Use of Truncated Flapped Airfoils for Impingement and Icing Tests of Full-Scale Leading-Edge Sections

Performance of a Short Combustor at High Altitudes Using Hydrogen Fuel

Investigation of the air-flow-regulation characteristics of a translating-spike inlet with two oblique shocks from Mach 1.6 to 2.0

Instrumentation for measurements of free-space sound pressures in the immediate vicinity of a propeller in flight

Interaction of grids with traveling shock waves

Initial results of a flight investigation of a gust-alleviation system

Investigation of plastic behavior of binary aluminum alloys by internal-friction methods

A method for obtaining statistical data on airplane vertical velocity at ground contact from measurements of center-of-gravity acceleration

The nickel dip : a radioisotope study of metallic deposits in porcelain enameling

Preliminary study of some factors which affect the stall-flutter characteristics of thin wings

Lift and moment coefficients for an oscillating rectangular wing-aileron configuration in supersonic flow

Measurement of aerodynamic forces for various mean angles of attack on an airfoil oscillating in pitch and on two finite-span wings oscillating in bending with emphasis on damping in the stall

Heat capacity lag of gaseous mixtures

Further measurements of intensity, scale, and spectra of turbulence in a subsonic jet

Effect of combustion-chamber pressure and nozzle expansion ratio on theoretical performance of several rocket propellant systems

The design of a miniature solid-propellant rocket

Effect of phosphate coatings on temperature of metal parts exposed to flame environments

Effect of pneumatic de-icers and ice formations on aerodynamic characteristics of a airfoil

Analytical study of modifications to the autopilot of a fighter airplane in order to reduce the response to side gusts

Comparison of landing-impact velocities of first and second wheel to contact from statistical measurements of transport airplane landings

Compressibility factor, density, specific heat, enthalpy, entropy, free-energy function, viscosity, and thermal conductivity of steam

Compressive crippling of structural sections

An analysis of estimated and experimental transonic downwash characteristics as affected by plan form and thickness for wing and wing-fuselage configurations

Experimental and calculated temperature and mass histories of vaporizing fuel drops

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