Browse TRAIL Inventories

A simplified method for assessing the effect of steady rolling on angle of attack and sideslip

A theoretical and experimental study of planing surfaces including effects of cross section and plan form

On possible similarity solutions for three-dimensional incompressible laminar boundary layers 3: similarity with respect to stationary polar coordinates for small angle variation

An investigation at low speed of the flow over a simulated flat plate at small angles of attack using pitot-static and hot-wire probes

A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry

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

Basic performance characteristics of several subsonic-diffuser-bypass-duct combinations for use with supersonic inlets

Two-dimensional cascade tests of NACA 65-(C(sub zeta)(sub o))A(sub 10))10 blade sections at typical compressor hub conditions for speeds up to choking

Preliminary investigation of dynamic lateral stability characteristics of a configuration of the North American X-15 research airplane

Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute

A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9

Theoretical rocket performance of JP-4 fuel with mixtures of liquid ozone and fluorine

Temperature measurements from a flight test of two wing-body combinations at 7 degree angle of attack for Mach numbers to 4.86 and Reynolds numbers to 19.2 X 10(exp 6)

Investigation of the planing lift of a flat plate at speeds up to 170 feet per second

Effect of bluntness on transition for a cone and a hollow cylinder at Mach 3.1

Free-flight investigation of jet effect on the low-lift drag and longitudinal trim of a supersonic interceptor-type airplane configuration with an overhanging tail boom at Mach numbers from 1.09 to 1.34

Experimental investigation of the forces and moments due to sideslip of a series of triangular vertical- and horizontal-tail combinations at Mach numbers of 1.62, 1.93, and 2.41

Propellant vaporization as a criterion for rocket-engine design : experimental effect of fuel temperature on liquid-oxygen - heptane performance

A study of injection processes for 15-percent fluorine - 85-percent oxygen and heptane in a 200-pound-thrust rocket engine

Aerodynamic heating of a thin, unswept, untapered, multiweb, aluminum-alloy wing at Mach numbers up to 2.67 as determined from a free-flight investigation of a rocket-propelled model

Performance of an experimental annular turbojet combustor with methane and propane

Vertical force-deflection characteristics of a pair of 56-inch-diameter aircraft tires from static and drop tests with and without prerotation

Investigation of the effects of propeller diameter on the ability of a flapped wing, with and without boundary-layer control, to deflect a propeller slipstream downward for vertical take-off

Supplementary Investigation in the Langley 20-Foot Free-Spinning Tunnel of a 1/20-Scale Model of the Douglas F4D-1 Airplane With External Wing Fuel Tanks

Effects of Extreme Surface Cooling on Boundary-Layer Transition

Some Effects of Aileron Deflection on the Static Lateral and Directional Aerodynamic Characteristics of Four Contemporary Airplane Models

Handbook of Structural Stability Part 2: Buckling of Composite Elements

Relation of Currently Estimated ANP Performance to Required ANP Performance

A Thermal System for Continuous Monitoring of Laminar and Turbulent Boundary-Layer Flows During Routine Flight

Attenuation in a Shock Tube Due to Unsteady-Boundary-Layer Action

The Mechanism of Thermal-Gradient Mass Transfer in the Sodium Hydroxide-Nickel System

Far Noise Field of Air Jets and Jet Engines

Full-Scale Investigation of Several Jet-Engine Noise-Reduction Nozzles

Elliptic Cones Alone and with Wings at Supersonic Speed

Growth of Disturbances in a Flame-Generated Shear Region

Theoretical and Experimental Investigation of the Subsonic-Flow Fields Beneath Swept and Unswept Wings with Tables or Vortex-Induced Velocities

Effect of Fatigue Crack on Static Strength: 2014-T6, 2024-T4, 6061-T6, 7075-T6 Open-Hole Monobloc Specimens

Some Observations on Stress-Corrosion Cracking of Single Crystals of AZ61X Magnesium Alloy

Some Factors Affecting the Static Longitudinal and Directional Stability Characteristics of Supersonic Aircraft Configurations

Identification of Foreign Objects Damaging Compressor Blades in Turbojet Engines

Propagation of Sound Into a Wind-Created Shadow Zone

Further Experiments on the Stability of Laminar and Turbulent Hydrogen-Air Flames at Reduced Pressures

Wind-Tunnel Flutter Tests at Mach Numbers Up to 3.0 of Boeing Wing Models for Weapons System 110A: Coord. No. AF-AM-108

Statistical Approach to the Estimation of Loads and Pressures on Seaplane Hulls for Routine Operations

Study of Some Burner Cross-Section Changes That Increase Space-Heating Rates

Study of Pressure Distributions on Simple Sharp-Nosed Models at Mach Numbers From 16 to 18 in Helium Flow

Summary of NACA Research on Ignition Lag of Self-Igniting Fuel - Nitric Acid Propellants

Tables of Various Mach Number Functions for Specific-Heat Ratios From 1.28 to 1.38

Appraisal of the Hazards of Friction-Spark Ignition of Aircraft Crash Fires

Investigation of an Air-Cooled, Plug-Type, Variable-Area Exhaust Nozzle


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