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Measurement of Flying Qualities of a DeHavilland Mosquito F-8 Airplane (AAF No. 43-334960) 2: Longitudinal Stability and Control Characteristics

Measurement of Flying Qualities of a Douglas A-26B Airplane (AAF No. 41-39120) 3: Stalling Characteristics

Investigation of Methods of Supporting Single-Thickness Specimens in a Fixture for Determination of Compressive Stress-Strain Curves

Knock-Limited Performance of Blends of AN-F-28 Fuel Containing 2 Percent Aromatic Amines 5

Lift Tests of a 0.1536c Thick Douglas Airfoil Section of NACA 7-Series Type Equipped With a Lateral-Control Device for Use With a Full-Span Double-Slotted Flap on the C-74 Airplane

Laboratory Investigation of Icing in the Carburetor and Supercharger Inlet Elbow of an Aircraft Engine 1: Description of Setup and Testing Technique

Knock-Limited Performance of Six Aromatic Amines Blended With a Base Fuel in a Full-Scale Aircraft-Engine Cylinder

Laboratory Investigation of Icing in the Carburetor and Supercharger Inlet Elbow of an Aircraft Engine 3: Heated Air as a Means of De-Icing the Carburetor and Supercharger Inlet Elbow

Laboratory Investigation of Icing in the Carburetor and Supercharger Inlet Elbow of an Aircraft Engine 5: Effect of Injection of Water-Fuel Mixtures and Water-Ethanol-Fuel Mixtures on the Icing Characteristics

Laboratory Investigation of Icing in the Carburetor and Supercharger Inlet Elbow of an Aircraft Engine 2: Determination of the Limiting-Icing Conditions

A New Apparatus for Measuring the Temperature at Machine Parts Rotating at High Speeds

The Minimum Energy Loss Propeller

Micromechanical Study of Metals

Airspeed Fluctuations as a Measure of Atmospheric Turbulence

Effects of Compressibility on the Maximum Lift Characteristics and Spanwise Load Distribution of a 12-Foot-Span Fighter-Type Wing of NACA 230-Series Airfoil Sections

In-Line Aircraft-Engine Bearing Loads 1: Crankpin-Bearing Loads

The Influence of Exhaust Pressure on Knock-Limited Performance

Flight Tests of the Sikorsky HNS-1 (Army YR-4B) Helicopter 2: Hovering and Vertical-Flight Performance With the Original and an Alternate Set of Main-Rotor Blades, Including a Comparison With Hovering Performance Theory

Full-scale-tunnel performance tests of the PV-2 helicopter rotor

"General" Main-Spray Tests of Flying-Boat Models in the Displacement Range

Flight Measurements of the Flying Qualities of an F6F-3 Airplane (BuAer No. 04776) 2: Lateral and Directional Stability and Control

Flight Measurements of the Flying Qualities of an F6F-3 Airplane (BuAer No. 04776) 3: Stalling Characteristics

Flight Measurements of the Flying Qualities of an F6F-3 Airplane (BuAer No. 04776) 1: Longitudinal Stability and Control

Flight Measurements of the Effect on Elevator Stick Forces of Stabilizer Incidence and Elevator Rib Spacing on the P-63A-1-BE Series Airplane

Flight Tests of a Rudder With a Spring Tab on an F6F-3 Airplane (BuAer No.04776)

Flight Tests of an SB2C-3 Airplane With a Production and Tilted Propeller Axis

Flight Tests of the Sikorsky HNS-1 (Army YR-4B) Helicopter 1: Experimental Data on Level-Flight Performance With Original Rotor Blades

Performance Characteristics of a Junkers Jumo 211F Engine Supercharger With a DVL Fully Shrouded Impeller and Scroll Diffuser

Comparative Fatigue Tests of Riveted Joints of Alclad 24S-T, Alclad 24S-T81, Alclad 24S-RT, Alclad 24S-T86 and Alclad 75S-T Sheet

Fatigue Strength of Flush-Riveted Joints for Aircraft Manufactured by Various Riveting Methods

Impact Properties at Different Temperatures of Flush-Riveted Joints for Aircraft Manufactured by Various Riveting Methods

A Metallurgical Investigation of a Large Forged Disc of Low-Carbon N-155 Alloy

Investigation of the NACA 4-(5)(08)-03 and NACA 4-(10)(08)-03 two-blade propellers at forward Mach numbers to 0.725 to determine the effects of camber and compressibility on performance

An Investigation of the Ranger V-770-8 Engine Installation for the Edo XOSE-1 Airplane 1: Cooling

A simple method for estimating terminal velocity including effect of compressibility on drag

Calculation of Centrally Loaded Thin-Walled Columns Above the Buckling Limit

Effect of fabric deflection at high speeds on the aerodynamic characteristics of the horizontal tail surface of an SB2D-1 airplane

Flight tests of two airplanes having moderately high effective dihedral and different directional stability and control characteristics

Ditching tests with a 1/16-size dynamic model of the Army B-24 airplane in Langley tank number 2 and on an outdoor catapult

Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface

The effect of afterbody length of the hydrodynamic stability of a dynamic model of a flying boat: Langley tank model 134

The effect of concentrated loads on flexible rings in circular shells

Comparison of fixed-stabilizer, adjustable- stabilizer and all-movable horizontal tails

Comparison of Pitching Moments Produced by Plain Flaps and by Spoilers and Some Aerodynamic Characteristics of an NACA 23012 Airfoil with Various Types of Aileron

Ditching behavior of military airplanes as affected by ditching aids

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

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


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