TRAIL - Technical Report Archive and Image Library

Fuel-Evaporation Loss as Determined by the Change in the Specific Gravity of the Fuel in an Aircraft Fuel Tank

An Investigation of a Thermal Ice-Prevention System for a C-46 Cargo Airplane 3: Description of Thermal Ice-Prevention Equipment for Wings, Empennage, and Windshield

Critical combinations of shear and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation

The development and application of high-critical-speed nose inlets

Analysis and modification of theory for impact of seaplanes on water

Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modifications of aileron nose and adjacent airfoil contour

Wind-Tunnel Tests of a Portion of a PV-2 Helicopter Rotor Blade

Wind-tunnel tests of spoilers on tail surfaces

Column and plate compressive strengths of aircraft structural materials: 17S-T aluminum-alloy sheet

Column and plate compressive strengths of aircraft structural materials: extruded 75S-T aluminum alloy

A flight investigation of NACA aileron modifications for the improvement of the lateral control characteristics of a high-speed fighter airplane

Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails

Flight investigation at high speeds of flow conditions over an airplane wing as indicated by surface tufts

Effects of compressibility on maximum lift coefficients for six propeller airfoils

Estimation of stick-fixed neutral points of airplanes

The effect of trailing-edge extension flaps on propeller characteristics

Bibliography and Review of Information Relating to the Hydrodynamics of Seaplanes

Bending and Shear Stresses Developed by the Instantaneous Arrest of the Root of a Cantilever Beam Rotating With Constant Angular Velocity About a Transverse Axis Through the Root

Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section

A summary of drag results from recent Langley full scale tunnel tests of Army and Navy airplanes

Summary of Airfoil Data

Statistical Analysis of the Characteristics of Repeated Gusts in Turbulent Air

Properties of low-aspect-ratio pointed wings at speeds below and above the speed of sound

Preliminary flight research on an all-movable horizontal tail as a longitudinal control for flight at high Mach numbers

Langley full-scale tunnel investigation of the factors affecting the directional stability and trim characteristics of a fighter-type

Performance of compressor-turbine jet-propulsion systems

A method of analysis of V-G records from transport operations

A Method of Analysis of V-G Records from Transport Operations

A method for the calculation of external lift, moment, and pressure drag of slender open-nose bodies of revolution at supersonic speeds

A method of analysis of V-G records from transport operations

A Metallurgical Investigation of a Large Forged Disc of 19-9 DL Alloy

A Metallurgical Investigation of a Large Forged Disc of CSA (234-A-5) Alloy

Addition of Heat to a Compressible Fluid in Motion

Pressure Lag in Tubing Used in Flight Research

The Elastic Constants for Wrought Aluminum Alloys

An Experimental Investigation of the Effect of Propellers Used as Aerodynamic Brakes on Stability and Control

Flight Tests of the Lateral Control Characteristics of an F6F-3 Airplane Equipped with Spring-Tab Ailerons

Correlation of Engine-Cooling Data

Effect of Internal Coolants on the Knock-Limited Performance of a Liquid-Cooled Multicylinder Aircraft Engine With a Compression Ratio of 6.0

The Effect of Some Design Parameters on Ditching Characteristics

Effect of the Lift Coefficient on Propeller Flutter

Effect of Maximum Cruise-Power Operation at Ultra-Lean Mixture and Increased Spark Advance on the Mechanical Condition of Cylinder Components

Effect of Mach and Reynolds Numbers on the Maximum Lift Coefficient Obtainable in Gradual and Abrupt Stalls of a Pursuit Airplane Equipped With a Low-Drag Wing

The Effect of Mach Number on the Aerodynamic Characteristics of a Single-Engine Pursuit Airplane as Determined From Tests of a 1/3-Scale Model

Effect of Variation in Diameter and Pitch of Rivets on Compressive Strength of Panels With Z-Section Stiffeners 1 - Panels With Close Stiffener Spacing That Fail by Local Buckling

Effect of Water-Alcohol Injection and Maximum Economy Spark Advance on Knock-Limited Performance and Fuel Economy of a Large Air-Cooled Cylinder

The Effect of Carburetor-Air Temperature on the Cooling Characteristics of a Typical Air-Cooled Engine Cylinder

An Estimate of the Effect of Engine Supercharging on the Take-Off Thrust of a Typical Helicopter at Different Altitudes and Temperatures

Estimation of F-3 and F-4 Knock-Limited Performance Ratings for Ternary and Quaternary Blends Containing Triptane or Other High-Antiknock Aviation-Fuel Blending Agents

Elimination of Galling of Pendulum-Vibration Dampers Used in Aircraft Engines

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