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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