Browse TRAIL Inventories

A Method for Estimating the Components of Lift of Wing-Body Combinations at Supersonic Speeds

Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems-Effect of Method of Positioning the Radar Antenna on the Speed of Response

General Correlation of Temperature Profiles Downstream of a Heated Air Jet Directed at Various Angles to Air Stream

Investigation at Mach Number 1.91 of Spreading Characteristics of Jet Expanding From Choked Nozzles

Effect of Design Changes of Operating Conditions on Combustion and Operational Performance of a 28-Inch Diameter Ram-Jet Engine

Analysis of a Nuclear-Powered Liquid-Metal Ducted-Fan Cycle

Analysis of a liquid-metal turbine-propeller cycle for propulsion of low-speed nuclear- powered aircraft

Radiant Heat Transfer From Flames in a Single Tubular Turbojet Combuctor

Wind-Tunnel Investigation of the Contribution of a Vertical Tail to the Directional Stability of a Fighter-Type Airplane

A Thermodynamic Study of the Turbine-Propeller Engine

A Low-Speed Investigation of an Annular Transonic Air Inlet

Radioautographic Method for Examining Distribution of Particles in a Cyclotron Beam

Effect of Temperatures From -70 to 600 Degrees Fahrenheit on Strength of Adhesive-Bonded Lap Shear Specimens of Clad 24S-T3 Aluminum Alloy and of Cotton-and Glass-Fabric Plastic Laminates

Several Combination Probes for Surveying Static and Total Pressure and Flow Direction

A Technique Applicable to the Aerodynamic Design of Inducer-Type Multistage Axial-Flow Compressors

Flight Investigation of Transient Wing Response on a Four-Engine Bomber Airplane in Rough Air With Respect to Center-of-Gravity Accelerations

Corrections for Lift, Drag, and Moment of an Airfoil in a Supersonic Tunnel Having a Given Static Pressure Gradient

X-Ray Instrumentation for Density Measurements in a Supersonic Flow Field

Supersonic Wave Drag of Nonlifting Delta Wings With Linearly Varying Thickness Ratio

Wind-Tunnel Investigation of the Effects of Various Asymmetric Canopy Modifications on the Behavior of Descending Parachutes

A Theoretical Method of Analyzing the Effects of Yaw-Damper Dynamics on the Stability of an Aircraft Equipped With a Second-Order Yaw Damper

An Impulse-Momentum Method for Calculating Landing-Gear Contact Conditions in Eccentric Landings

The Effect of a Simulated Propeller Slipstream on the Aerodynamic Characteristics of an Unswept Wing Panel With and Without Nacelles at Mach Numbers From 0.30 to 0.86

Estimation of the Maximum Angle of Sideslip for Determination of Vertical-Tail Loads in Rolling Maneuvers

Experimental Determination of Time Constants and Nusselt Numbers for Bare-Wire Thermocouples in High-Velocity Air Streams and Analytic Approximation of Conduction and Radiation Errors

The Effect of Blade-Section Camber on the Static Characteristics of Three NACA Propellers

Interaction of Column and Local Buckling in Compression Members

Short-Bearing Approximation for Full Journal Bearings

Correlation of Tensile Strength, Tensile Ductility, and Notch Tensile Strength With the Strength of Rotating Disks of Several Designs in the Range of Low and Intermediate Ductility

Bending of Thin Plates With Compound Curvature

Buckling of Low Arches or Curved Beams of Small Curvature

A Low-Speed Investigation of a Fuselage-Side Air Inlet for Use at Transonic Flight Speeds

Inviscid Flow About Airfoils at High Supersonic Speeds

Influence of Lubricant Viscosity on Operating Temperatures of 75-Millimeter-Bore Cylindrical-Roller Bearing at High Speeds

The Gust and Gust-Load Experience of a Twin-Engine Low-Altitude Transport Airplane in Operation on a Northern Transcontinental Route

Experiments in External Noise Reduction of a Small Pusher-Type Amphibian Airplane

Experiments to Determine Neighborhood Reactions to Light Airplanes With and Without External Noise Reduction

On the Representation of the Stability Region in Oscillation Problems With the Aid of the Hurwitz Determinants

Preliminary Air-Flow and Thrust Calibrations of Several Conical Cooling-Air Ejectors with a Primary to Secondary Temperature Ratio of 1.0, 2: Diameter Ratios of 1.06 and 1.40

The Effect of High Viscosity on the Flow Around a Cylinder and Around a Sphere

Translational Motion of Bodies Under the Free Surface of a Heavy Fluid of Finite Depth

Structural Vulnerability of the Boeing B-29 Aircraft Wing to Damage by Warhead Fragments

A Theoretical Analysis of the Effects of Fuel Motion on Airplane Dynamics

Wind-Tunnel Investigation of the Low-Speed Static Stability and Control Characteristics of a Model of the Bell MX-776 (RASCAL) in Combined Angle of Attack and Sideslip

Pressure Recovery, Drag, and Subcritical Stability Characteristics of Conical Supersonic Diffusers With Boundary-Layer Removal

Investigation in the Ames Supersonic Free-Flight Wind Tunnel of the Static Longitudinal Stability of the Hermes A-3B Missile at a Mach Number of 5.0

Method for Calculation of Laminar Heat Transfer in Air Flow Around Cylinders of Arbitrary Cross Section (Including Large Temperature Differences and Transpiration Cooling)

A Wind-Tunnel Investigation to Determine the Effect of Various Head Designs on the Aerodynamic Characteristics in Pitch of the Army Ordnance Corps T205 3.5-Inch Heat Rocket

Investigation of Spinning and Tumbling Characteristics of a 1/20-Scale Model of the Consolidated Vultee XFY-1 Airplane in the Free-Spinning Tunnel, TED No. NACA DE 370

Preliminary Results Obtained from Flight Test of a 1/7-Scale Rocket-Powered Model of the Grumman XF10F Airplane Configuration in the Swept-Wing Condition, TED No. NACA DE 354


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