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- Wind-tunnel investigation of 20-percent-chord plain and Frise ailerons on an NACA 23012 airfoil
- Wind-Tunnel Investigation of Perforated Split Flaps for Use as Dive Brakes on a Tapered NACA 23012 Airfoil
- Aerodynamic Characteristics and Flap Loads of the Brake-Flap Installation on the 0.40-Scale Model of the F4F-3 Left Wing Panel
- A study of the application of data on various types of flap to the design of fighter brakes
- Wind-Tunnel Investigation of Control-Surface Characteristics 15: Various Contour Modifications of a 0.30-Airfoil-Chord Plain Flap on an NACA 66(215)-014 Airfoil
- Wind-Tunnel Investigation of a Plain Aileron with Various Trailing-Edge Modifications on a Tapered Wing 3: Ailerons with Simple and Spring-Linked Balancing Tabs
- Wind-Tunnel Investigation of an NACA 23012 Airfoil With a 0.30-Airfoil-Chord Double Slotted Flap
- Wind-tunnel investigation of a plain aileron with thickened and beveled trailing edges on a tapered low-drag wing
- Wind-Tunnel Investigation of the Characteristics of Blunt-Nose Ailerons on a Tapered Wing
- Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails
- Analysis of Available Data on Control Surfaces Having Plain-Overhang and Frise Balances
- Effects of trailing-edge modifications on pitching moment characteristics of airfoils
- 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
- Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails
- Tests to Determine Effects of Slipstream Rotation on the Lateral Stability Characteristics of a Single-Engine Low-Wing Aircraft Model
- Wind-Tunnel Investigation of Effects of Unsymmetrical Horizontal-Tail Arrangements on Power-on Static Longitudinal Stability of a Single-Engine Airplane Model
- Collection and Analysis of Hinge-Moment Data on Control-Surface Tabs
- Preliminary investigation at low speed of downwash characteristics of small-scale sweptback wings
- Wind-Tunnel Tests at Low Speed of Swept and Yawed Wings Having Various Plan Forms
- Flight Tests of Rocket-Powered "Tin-Can" Models of AAF Project MX-800
- Effect of a pilot's canopy on the drag of an NACA RM-2 drag research model in flight at transonic and supersonic speeds