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Calculation of Turbulent Expansion Processes

Charts for the Minimum-Weight Design of 24S-T Aluminum-Alloy Flat Compression Panels With Longitudinal Z-Section Stiffeners

Data for Design of Entrance Vanes from Two-Dimensional Tests of Airfoils in Cascade

Correlation of Exhaust-Valve Temperatures With Engine Operating Conditions and Valve Design in an Air-Cooled Cylinder

Completed Tabulation in the United States of Tests of 24 Airfoils at High Mach Numbers (Derived From Interrupted Work at Guidonia, Italy in the 1.31- by 1.74-Foot High-Speed Tunnel)

On Two-Dimensional Flows of Compressible Fluids

Heat-Transfer Tests of Aqueous Ethylene Glycol Solutions in an Electrically Heated Tube

Heat-Transfer Coefficients for Air Flowing in Round Tubes, in Rectangular Ducts, and Around Finned Cylinders

Stresses at Cut-Outs in Shear Resistant Webs as Determined by the Photoelastic Method

On a Method of Constructing Two-Dimensional Subsonic Compressible Flows Around Closed Profiles

On the Circulatory Subsonic Flow of a Compressible Fluid Past a Circular Cylinder

The Chemical Action of Oils on Single Crystals of Metals

Tests on Thin-Walled Celluloid Cylinders to Determine the Interaction Curves Under Combined Bending, Torsion, and Compression or Tension Loads

Graphical and Analytical Methods for the Determination of a Flow of a Compressible Fluid Around an Obstacle

Effect of Propeller-Axis Angle of Attack on Thrust Distribution Over the Propeller Disk in Relation to Wake-Survey Measurement of Thrust

Studies of Blade Shank and Pitch Distribution for Constant-Speed Propellers

Survey of Adhesives and Adhesion

Effect of Fatigue-Stressing Short of Failure on Some Typical Aircraft Metals

Axial Fatigue Test at Two Stress Amplitudes of 0.032-Inch 24S-T Sheet Specimens With a Circular Hole

Flight Tests of Dive-Recovery Flaps on an XP-51 Airplane

Nitrous Oxide Supercharging of an Aircraft-Engine Cylinder

Piston-Ring Vibration and Breakage

A Preignition Indicator for Aircraft Engines

On the Shear Strength of Skin-Stiffener Panels With Inspection Cut-Outs

Operating Stresses in Aircraft-Engine Crankshafts and Connecting Rods 1: Slip-Ring and Bush Combinations for Dynamic-Strain Measurements

Flight and Test-Stand Investigation of High-Performance Fuels in Modified Double-Row Radial Air-Cooled Engines 1: Determination of the Cooling Characteristics of the Flight Engine

Flight and Test-Stand Investigation of High-Performance Fuels in Modified Double-Row Radial Air-Cooled Engines 2: Flight Knock Data and Comparison of Fuel Knock Limits With Engine Cooling Limits in Flight

Tensile-Strength Investigation of Cast-Iron Piston Rings of Various Strengths

Tank Tests of a Flying-Boat Model Equipped With Several Types of Fairing Designed to Reduce the Air Drag of the Main Step

Tank Tests of a Powered Dynamic Model of a Flying Boat Having an Afterbody Length-Beam Ratio of 4.7-Langley Tank Model 203C-1

Spray Characteristics and Take-Off and Landing Stability of Several Modifications of a 1/8-Size Model of the PBN-1 Flying Boat - NACA Model 192

Stability and Control Characteristics of a Fighter Airplane in Inverted Flight Attitude as Determined by Model Tests

Shear-Lag Tests of a Box Beam With a Highly Cambered Cover in Tension

Performance Selection Charts for Gliders and Twin-Engine Tow Planes

Reduction of Fuel-Vapor Loss by Omitting Some of the Fuel Constituents Normally Lost During Flight

Tunnel-Wall Corrections to Rolling and Yawing Moments Due to Aileron Deflection in Closed Rectangular Wind Tunnels

The Two-Dimensional Incompressible Potential Flow Over Corrugated and Distorted Infinite Surfaces

Ultraviolet Absorption Spectra of Aromatic Amines in Isooctane and in Water

Two-Dimensional Wind-Tunnel Investigation of Spoiler Aileron Flap Model for the Hughes XF-11 Airplane

Two-Dimensional Wind-Tunnel Investigation of Six Airfoil Sections for the Wing of the Vega XP2V-1 Airplane

Radial Aircraft-Engine Bearing Loads 1: Crankpin-Bearing Loads for Engines Having Nine Cylinders Per Crankpin

Recent Development of the Two-Stroke Engine 2 - Design Features

Relation Between Fuel Economy and Crank Angle for the Maximum Rate of Pressure Rise

Response of Helicopter Rotors to Periodic Forces

Resistance Tests of Models of Three Flying-Boat Hulls With a Length-Beam Ratio of 10.5

The Resistance of Three Series of Flying Boat-Hulls as Affected by Length-Beam Ratio

Static-Thrust Tests of Six Rotor-Blade Designs on a Helicopter in the Langley Full-Scale Tunnel

Strain Measurements and Strength Tests on the Tension Side of a Box Beam With Flat Cover

Stresses Near the Juncture of a Closed and an Open Torsion Box as Influenced by Bulkhead Flexibility

Study of the Mixture Distribution of a Double-Row Radial Aircraft Engine


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