TRAIL - Technical Report Archive and Image Library

Analysis of Multicell Delta Wings on Cal-Tech Analog Computer

An Analytical Investigation of the Effect of the Rate of Increase of Turbulent Kinetic Energy in the Stream Direction on the Development of Turbulent Boundary Layers in Adverse Pressure Gradients

The Condensation Line of Air and the Heats of Vaporization of Oxygen and Nitrogen

Some Problems on the Theory of Creep

A New Simple Interferometer for Obtaining Quantitatively Evaluable Flow Patterns

On Transonic Flow Past a Wave-Shaped Wall

On the Theory of the Turbulent Boundary Layer

Cooperative Investigation of Relationship Between Static and Fatigue Properties of Wrought N-155 Alloy at Elevated Temperatures

Supersaturation in the Spontaneous Formation of Nuclei in Water Vapor

The Microstructure of Turbulent Flow

Plastic Deformation of Aluminum Single Crystals at Elevated Temperatures

Concerning the Flow About Ring-Shaped Cowlings 12: Two New Classes of Circular Cowls

Steady Vibrations of Wing of Circular Plan Form

Concerning the Flow on Ring-Shaped Cowlings Part 13: The Influence of a Projecting Hub

Calculation of the Shape of a Two-Dimensional Supersonic Nozzle in Closed Form

Deflection and Stress Analysis of Thin Solid Wings of Arbitrary Plan Form with Particular Reference to Delta Wings

One-Dimensional Analysis of Choked-Flow Turbines

Theoretical Prediction of Pressure Distributions on Nonlifting Airfoils at High Subsonic Speeds

Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems: Effect of Missile Configuration on the Speed of Response

A Method for Estimating the Rolling Moments Caused by Wing-Tail Interference for Missiles at Supersonic Speeds

Investigation of Pressure Recovery of a Single-Conical-Shock Nose Inlet at Mach Number 5.4

Weight Bar Charts

Criticality Survey of Hydroxides as Coolant Moderators for Aircraft Nuclear Reactors

Summary Report on Analytical Evaluation of Air and Fuel Specific-Impulse Characteristics of Several Nonhydrocarbon Jet-Engine Fuels

Static Longitudinal Stability and Control Characteristics of a 1/16 -Scale Model of the Douglas D-558-II Research Airplane at Mach Numbers of 1.61 and 2.01

Performance Characteristics of a Double-Cylindrical-Shroud Ejector Nozzle

Wind-Tunnel Investigation of the Motion of a 1/10-Scale Model of the Douglas XF4D-1 Escape Capsule When Jettisoned by Jet Ejection: TED No. NACA DE 359

The Low-Speed Lift and Drag Characteristics of a Series of Airplane Models Having Triangular or Modified Triangular Wings

Damping in Pitch of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds

Effect of Large Deflection of a Canard Control and Deflections of a Wing-Tip Control on the Static-Stability and Induced-Roll Characteristics of a Cruciform Canard Missile at a Mach Number of 2.01

Effects of External Store Mounting on the Buffet, Trim, and Drag Characteristics of Rocket-Powered Fuselage and Store Combinations Between Mach Numbers of 0.7 and 1.4

Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine 13: Endurance Evaluation of Several Protective Coatings Applied to Turbine Blades of Nonstrategic Steels

Effects of Span and Spanwise and Chordwise Location on the Control Effectiveness of Spoilers on a 50 Degree Sweptback Wing at Mach Numbers of 1.41 and 1.96

Equations, Tables, and Charts for Compressible Flow

A Compilation of Summaries From NACA Reports on Fuels Research, 1945-1952

Effect of Capture on the Slowing-Down Length of Neutrons in Hydrogenous Mixtures Containing Uranium

Transonic Flow Past Cone Cylinders

Investigation of an Axial-Flow-Compressor Rotor With Circular-Arc Blades Operating Up to a Rotor-Inlet Relative Mach Number of 1.22

Preliminary Experiments with Pilot Burners for Ram-Jet Combustors

Preliminary Investigation of the Effects of Cascading on the Oscillating Lift Force of an Airfoil Vibrated in Bending

Supersonic Flow Past Oscillating Airfoils Including Nonlinear Thickness Effects

Correlation by the Hypersonic Similarity Rule of the Pressure Distributions and Wave Drags for Minimum-Drag Nose Shapes at Zero Angle of Attack

A Transonic Wind-Tunnel Investigation of the Effect of Modifications to an Indented Body in Combination With a 45 Degree Sweptback Wing

A Transonic Wind-Tunnel Investigation of the Effects of Longitudinal Wing Location and Varying Body Size on the Interference Characteristics of a 45 Degrees Sweptback Wing

Correlation of Flight and Wind-Tunnel Measurements of Roll-Off in Low-Speed Stalls on a 35 Degree Swept-Wing Aircraft

Dynamic Characteristics of a Single-Spool Turbojet Engine

Preliminary Results of an Investigation of the Effects of Spinner Shape on the Characteristics of an NACA D-Type Cowl Behind a Three-Blade Propeller, Including the Characteristics of the Propeller at Negative Thrust

Transverse Vibrations of Hollow Thin-Walled Cylindrical Beams

Investigation of Aerodynamic and Icing Characteristics of a Flush Alternate-Inlet Induction-System Air Scoop

Altitude Investigation of Several Afterburner Configurations for the J40-WE-8 Turbojet Engine

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