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An empirical formula for the critical shear stress of curved sheets

Summary of measurements in Langley full-scale tunnel of maximum lift coefficients and stalling characteristics of airplanes

Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 24S-T Aluminum Alloy

Column and plate compressive strengths of aircraft structural materials: extruded 24S-T aluminum alloy

Comparison between calculated and measured loads on wing and horizontal tail in pull-up maneuvers

Comparison of wind-tunnel and flight measurements of stability and control characteristics of a Douglas A-26 airplane

The effect of high loading on landing technique and distance, with experimental data for the B-26 airplane

Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

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

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

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

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

Net Heat of Combustion of AN-F-28 Aviation Gasolines

Effect of normal pressure on the critical compressive and shear stress of curved sheet

Bending-Torsion Flutter Calculations Modified by Subsonic Compressibility Corrections

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

The Use of Geared Spring Tabs for Elevator Control

Visual Studies of Cylinder Lubrication [Part] 1: The Lubrication of the Piston Skirt

Wind-Tunnel Investigation of the Effects of Spoilers on the Characteristics of a Low-Drag Airfoil Equipped With a 0.25-Chord Slotted Flap

Effect of the Performance of a Turbosupercharged Engine of an Exhaust-Gas-to-Air Heat Exchanger for Thermal Ice Prevention

Calculations of Economy of 18-Cylinder Radial Aircraft Engine With Exhaust-Gas Turbine Geared to the Crankshaft at Cruising Speed

An Investigation of Aircraft Heaters 18: A Design Manual for Exhaust Gas and Air Heat Exchangers

The Knock-Limited Performance of S Reference Fuel Plus 2 Milliliters of Triethylthallium Per Gallon

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


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