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Simplified Propeller Design for Low-Powered Airplanes

Propeller Scale Effect and Body Interference

Propeller Design: Practical Application of the Blade Element Theory 1

Propeller Design: Extension of Test Data on a Family of Model Propellers by Means of the Modified Blade Element Theory 2

Propeller Design - A Simple Method for Determining the Strength of Propellers - IV

Navy Propeller Section Characteristics as Used in Propeller Design

Study of Open Jet Wind Tunnel Cones

Full Scale Tests of Wood Propellers on a VE-7 Airplane in the Propeller Research Tunnel

Drag and Cooling With Various Forms of Cowling for A "Whirlwind" Radial Air-Cooled Engine - 2

Drag and Cooling With Various Forms of Cowling for A "Whirlwind" Radial Air-Cooled Engine - 1

Full Scale Tests on a Thin Metal Propeller at Various Tip Speeds

Full-Scale Wind-Tunnel Tests of a Series of Metal Propellers on a VE-7 Airplane

Full Scale Drag Tests on Various Parts of Sperry Messenger Airplane

Drag and Cooling With Various Forms of Cowling for a Whirlwind Engine in a Cabin Fuselage

The Drag of a J-5 Radial Air-Cooled Engine

The Effect of the Sperry Messenger Fuselage on the Air Flow at the Propeller Plane

Determination of Propeller Deflection by Means of Static Load Tests on Models

A Comparison of Propeller and Centrifugal Fans for Circulating the Air in a Wind Tunnel

The Effect of Reduction Gearing on Propeller-Body Interference as Shown by Full-Scale Wind-Tunnel Tests

Full-Scale Wind-Tunnel Tests on Several Metal Propellers Having Different Blade Forms

Full-Scale Wind-Tunnel Tests With a Series of Propellers of Different Diameters on a Single Fuselage

Working Charts for the Selection of Aluminum Alloy Propellers of a Standard Form to Operate With Various Aircraft Engines and Bodies

The twenty-foot propeller research tunnel of the National Advisory Committee for Aeronautics

Tests of Four Racing Type Airfoils in the Twenty-Foot Propeller Research Tunnel

Full Scale Investigation of the Drag of a Wing Radiator

The effect of the wings of single engine airplanes on propulsive efficiency as shown by full scale wind tunnel tests


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