TRAIL - Technical Report Archive and Image Library

Calibration of Three Temperature Probes and a Pressure Probe at High Speeds

Jet-Boundary Corrections to the Downwash Behind Powered Models in Rectangular Wind Tunnels With Numerical Values for 7- by 10-Foot Closed Wind Tunnels

Wind-Tunnel Investigation of an NACA 23012 Airfoil with a Handley Page Slat and Two Flap Arrangements

Cooling Investigation of a B-24D Engine-Nacelle Installation in the NACA Full-Scale Tunnel

Effect of Changes in Aspect Ratio, Side Area, Flight-Path Angle, and Normal Acceleration on Lateral Stability

Determination of the Stability and Control Characteristics of Airplanes from Tests of Powered Models

Tests of a Large Spherical Turret and a Modified Turret on a Typical Bomber Fuselage

Control of Torsional Vibrations by Pendulum Masses

The Compressible Potential Flow Past Elliptic Symmetrical Cylinders at Zero Angle of Attack and with No Circulation

Effect of Normal Pressure on the Critical Compressive Stress of Curved Sheet

Effects of Range of Stress and of Special Notches on Fatigue Properties of Aluminum Alloys Suitable for Airplane Propellers

The Tracer Gas Method of Determining the Charging Efficiency of Two-Stroke-Cycle Diesel Engines

The Limiting Useful Deflections of Corrugated Metal Diaphragms

Investigation of the Forces Acting on Gliders in Automobile-, Pulley-, Winch-, and Airplane Towed Flight

Curing of Resin-Wood Combinations by High-Frequency Heating

Improvement of Fatigue Life of an Aluminum Alloy by Overstressing

Stress Analysis of Monocoque Fuselage Bulkheads by the Photoelastic Method

A Rosette Strain Computer

A Preliminary Investigation of the Electrical Structure of Thunderstorms

A Method for Determining the Camber and Twist of a Surface to Support a Given Distribution of Lift

Tidewater and Weather-Exposure Tests on Metals Used in Aircraft - 2

On the Distribution of Stress in a Thin Plate Elastically Supported Along Two Edges at Loads Beyond the Stability Limit

Tensile and Pack Compressive Tests of Some Sheets of Aluminum Alloy, 1025 Carbon Steel, and Chromium-Nickel Steel

Tests of Propeller-Speed Cooling Blowers

Investigation of Lubricants Under Boundary Friction

Propeller Selection From Aerodynamic Considerations

On the Symmetrical Potential Flow of Compressible Fluid Past a Circular Cylinder in the Tunnel in the Subcritical Zone

Progress Summary Number 1: Mechanical Properties of Flush-Riveted Joints Submitted by Five Airplane Manufacturers

Flight Tests of Modifications to Improve the Aileron Control Characteristics of a North American XP-51 Airplane (AC No. 41-38)

Wind-tunnel investigation of an NACA full-span high-lift lateral-control combination 1: section characteristics, NACA 23012 airfoil

Wind-tunnel investigation of control-surface characteristics 5: the use of a beveled trailing edge to reduce the hinge moment of a control surface

Wind-tunnel investigation of control-surface characteristics 8: a large aerodynamic balance of two nose shapes used with a 30-percent-chord flap on an NACA 0015 airfoil

A flight investigation of short-period longitudinal oscillations of an airplane with free elevator

Flight investigation of the performance and cooling characteristics of a long-nose high-inlet-velocity cowling on the XP-42 airplane

Flight investigation of an NACA ice-detector suitable for use as a rate-of-icing indicator

A flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap

An Experimental Investigation of Flow Across Tube Banks

An Investigation of Hydrofoils in the NACA Tank 1: Effect of Dihedral and Depth of Submersion

Interference effects of longitudinal flat plates on low-drag airfoils

Flight investigation of a stall-warning indicator for operation under icing conditions

Generalized selection charts for bombers powered by one, two, four, and six 2000-horsepower engines

Graphical representation of intercooler parameters and performance at altitudes from 25,000 to 60,000 feet

High-speed tests of radial-engine nacelles on a thick low-drag wing

The strength of plane web systems in incomplete diagonal tension

A study of the effect of adverse yawing moment on lateral maneuverability at a high lift coefficient

Pressure-Distribution Measurements of a Model of a Davis Wing Section with Fowler Flap Submitted by Consolidated Aircraft Corporation

A study of the application of data on various types of flap to the design of fighter brakes

Pressure-distribution measurements of two airfoil models with Fowler flaps submitted by Consolidated Aircraft Corporation as alternative wing sections of the XB-32 airplane

Preliminary experimental investigation of airfoils in cascade

A preliminary investigation of exhaust-gas ejectors for ground cooling

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