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Charts for Determining Propeller Efficiency

Dynamic Loads on Airplane Structures During Landing

Effect of Developed Width on Strength of Axially Loaded Curved Sheet Stringer Panels

Investigation of the Behavior of Parallel Two-Dimensional Air Jets

An Investigation of the Characteristics of Alcohol-Distribution Tubes Used for Ice Protection on Aircraft Windshields

Wind-Tunnel Investigation of a 1/20-Scale Powered Model of a Four-Engine Transport Airplane

Performance of NACA Eight-Stage Axial-Flow Compressor at Simulated Altitudes

Performance Characteristics of Journal Bearings With Forced-Feed Lubrication

An Experimental Investigation of the Thrust and Torque Produced by Propellers Used as Aerodynamic Brakes

Investigation of Effect of Sideslip on Lateral Stability Characteristics 1: Circular Fuselage with Variations in Vertical-Tail Area and Tail Length With and Without Horizontal Tail Surface

High Temperature Characteristics of 17 Alloys at 1200 and 1350 Degrees F

The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA Free-Flight Tunnel

Effect of a Trailing-Edge Extension on the Characteristics of a Propeller Section

Simple Curves for Determining the Effects of Compressibility on Pressure Drop Through Radiators

High-Altitude Cooling 3: Radiators

Effect of Fuel Volatility on Performance of a Wright R-2600-8 Engine as Influenced by Mixture Distribution

Wind-Tunnel Investigation of Carburetor Air Scoops for the XTB2D-1 Airplane with Emphasis on Means for Bypassing the Boundary Layer

Wind-Tunnel Investigation of Ailerons on a Low-Drag Airfoil 3: The Effect of Tabs

The Effect of Engine Conditions on the Lead Susceptibility of Paraffinic Fuels

Experimental Study of the Coating Found on Scuffed Cast-Iron Piston Rings During Operation in Nitrided-Steel Cylinders

Wind-Tunnel Investigation of a Beveled Aileron Shape Designed to Increase the Useful Deflection Range

Tests of NACA 65(216)-420 and 66(218)-420 Airfoils at High Speeds

Cylinder-Head Cooling by Means of a Shield in the Exhaust Passage

Air-Consumption Parameters for Automatic Mixture Control of Aircraft Engines

Determination of the Stresses Produced by the Landing Impact in the Bulkheads of a Seaplane Bottom

Comparative Results of Tests on Several Different Types of Nozzles

Compressibility Effects on Heat Transfer and Pressure Drop in Smooth Cylindrical Tubes

Determination of the Actual Contact Surface of a Brush Contact

DVL Angular Velocity Recorder

Simply Supported Long Rectangular Plate Under Combined Axial Load and Normal Pressure

On the General Theory of Thin Airfoils for Nonuniform Motion

The "Limiting Line" in Mixed Subsonic and Supersonic Flow of Compressible Fluids

Dynamics of the Inlet System of a Four-Stroke Engine

The Conformal Transformation of an Airfoil Into a Straight Line and Its Application to the Inverse Problem of Airfoil Theory

The Influence of the Aerodynamic Span Effect on the Magnitude of the Torsional-Divergence Velocity and on the Shape of the Corresponding Deflection Mode

Fairing Compositions for Aircraft Surfaces

The Effect of Increased Cooling Surface on Performance of Aircraft-Engine Cylinders as Shown by Tests of the NACA Cylinder

Wind-Tunnel Tests of the 1/8-Scale Powered Model of the Curtiss XBTC-2 Airplane 1: Preliminary Investigation of Longitudinal Stability

Ovalization of Tubes Under Bending and Compression

Power-Off Tests of the Northrop N9M-2 Tailless Airplane in the 40- by 80-Foot Wind Tunnel

High-Altitude Cooling 3: Radiators

Flight Tests of the High-Speed Performance of a P-51B Airplane (AAF No. 43-12105)

Applicability of Similarity Principles to Structural Models

A Least-Squares Procedure for the Solution of the Lifting-Line Integral Equation

Piloting of flying boats with special reference to porpoising and skipping

Notes on Unusual V-G Records From Transport Airplanes

The Effect of Increased Cooling Surface on Performance of Aircraft-Engine Cylinders as Shown by Tests of the NACA Cylinder

A Comparison of the Effects of Four-Blade Dual- and Single-Rotation Propellers on the Stability and Control Characteristics of a High-Powered Single-Engine Airplane

Performance of Blowdown Turbine Driven by Exhaust Gas of Nine-Cylinder Radial Engine

Preliminary Investigation of the Relation of the Compressive Strength of Sheet-Stiffener Panels to the Diameter of Rivet Used for Attaching Stiffeners to Sheet


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