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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
- 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 Tests of Wood Propellers on a VE-7 Airplane in the Propeller Research Tunnel
- 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
- Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack 1: Ordinary Ailerons on Rectangular Wings
- The Behavior of Conventional Airplanes in Situations Thought to Lead to Most Crashes
- The Characteristics of a Clark Y Wing Model Equipped With Several Forms of Low-Drag Fixed Slots
- Preliminary Investigation of Modifications to Conventional Airplanes to Give Nonstalling and Short-Landing Characteristics
- Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack 3: Ordinary Ailerons Rigged Up 10 Degrees When Neutral
- Wind-Tunnel Tests of a Clark Y Wing With a Narrow Auxiliary Airfoil in Different Positions
- Wind-tunnel research comparing lateral control devices, particularly at high angles of attack 4: floating tip ailerons on rectangular wings
- Wind-tunnel research comparing lateral control devices, particularly at high angles of attack 6: skewed ailerons on rectangular wings
- Wind-tunnel research comparing lateral control devices, particularly at high angles of attack 2: slotted ailerons and frise ailerons
- The Aerodynamic Characteristics of a Model Wing Having a Split Flap Deflected Downward and Moved to the Rear
- Wind-Tunnel Tests of a Hall High-Life Wing
- Wind-tunnel tests of the Fowler variable-area wing
- Preliminary Investigation of Rolling Moments Obtained With Spoilers on Both Slotted and Plain Wings
- Effect of Length of Handley Page Tip Slots on the Lateral-Stability Factor, Damping in Roll
- The effect of multiple fixed slots and a trailing-edge flap on the lift and drag of a Clark Y airfoil
- Wind-tunnel research comparing lateral control devices, particularly at high angles of attack V : spoilers and ailerons on rectangular wings
- Wind-Tunnel Tests on Combinations of a Wing With Fixed Auxiliary Airfoils Having Various Chords and Profiles
- Present Status of Lateral-Control Devices for Use With Split Flaps, Special Report
- Flight Tests on the Lateral Control of an Airplane having a Split Flap which Retracts Ahead of Conventional Ailerons, Special Report
- Aerodynamic tests of a low aspect ratio tapered wing with various flaps, for use on tailless airplanes
- Wind Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack 8: Straight and Skewed Ailerons on Wings With Rounded Tips
- Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack 9: Tapered Wings With Ordinary Ailerons
- The effect on lift, drag, and spinning characteristics of sharp leading edges on airplane wings
- Wind tunnel research comparing lateral control devices, particularly at high angles of attack 10: various control devices on a wing with a fixed auxiliary airfoil