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• Observations of the Improvement in Vision Brought About by the Application of a Rain-Repellent Lacquer on an Airplane Windshield
• Radiator Design and Installation - 2
• Stresses Around Rectangular Cut-Outs in Skin-Stringer Panels Under Axial Loads
• Strength Tests of Thin-Wall Truncated Cones of Circular Section
• Study of Turning Performance of a Fighter-Type Airplane Particularly as Affected by Flaps and Increased Supercharging, Special Report
• Preliminary Wind-Tunnel Tests of the Effect of Nacelles on the Characteristics of a Twin-Engine Bomber Model with Low-Drag Wing, Special Report
• The Problem of Thermal-Expansion Stresses in Reinforced Plastics
• Some Lift and Drag Measurements of a Representative Bomber Nacelle on a Low-Drag Wing
• Some Lift and Drag Measurements of a Representative Bomber Nacelle on a Low-Drag Wing 2
• The Stability of Laminar Flow Past a Sphere
• Wind-Tunnel Development of Ailerons for the Curtiss XP-60 Airplane, Special Report
• Analytical Theory of the Campini Propulsion System
• Wind-Tunnel Tests of Four- and Six-Blade Single- and Dual-Rotating Tractor Propellers
• Theoretical Solution of Profile Drag
• Tests of a Highly Cambered Low-Drag-Airfoil Section with a Lift-Control Flap, Special Report
• Tests of an NACA 66,2-420 Airfoil of 5-Foot Chord at High Speed, Special Report
• Thermal Theory of Combustion and Explosion 3: Theory of Normal Flame Propagation
• [Memorandums on the Subject of Turbulent Boundary Layers in Compressible Gas at High Speeds]
• The Formation of Ice on Aircraft
• The Icing of Aircraft
• The Longitudinal Stability of Flying Boats as Determined by Tests of Models in the NACA Tank 2: Effect of Variations in Form of Hull on Longitudinal Stability
• Cooling in Cruising Flight With Low Fuel-Air Ratios
• Effects of Direction of Propeller Rotation on the Longitudinal Stability of the 1/10-Scale Model of the North American XB-28 Airplane With Flaps Neutral
• Drag and Propulsive Characteristics of Air-Cooled Engine-Nacelle Installations for Large Airplane
• The Effect of Cowling Shape on the Stability Characteristics of an Airplane
• Recent Results in Rocket Flight Technique
• The Effect of Solidity, Blade Section, and Contravane Angle on the Characteristics of an Axial-Flow Fan
• Analysis of Heat and Compressibility Effects in Internal Flow Systems and High-Speed Tests of a Ram-Jet System
• Cooling Tests of an Air-Cooled Engine Cylinder With Copper Fins on the Barrel
• Contribution to the Design of Plywood Shells
• Aerodynamics of the Fuselage
• A Brief Study of the Speed Reduction of Overtaking Airplanes by Means of Air Brakes
• Generalized Selection Charts for Harrison and Tubular Intercoolers
• The Performance of a Vaneless Diffuser Fan
• The Navier-Stokes Stress Principle for Viscous Fluids
• Two-Dimensional Potential Flow Past an Ordinary Thick Wing Profile
• Wind-Tunnel Investigations of Diving Brakes
• Theory of Heat Transfer in Smooth and Rough Pipes
• Application of Balancing Tabs to Ailerons
• Aerodynamic Characteristics and Flap Loads of the Brake-Flap Installation on the 0.40-Scale Model of the F4F-3 Left Wing Panel
• Adjustment of Stick Force by a Nonlinear Aileron-Stick Linkage
• Aerodynamic Characteristics for Internal-Balance and Frise Type Ailerons on an NACA 6 Series Low-Drag Tip Section of the Wing for the XP-63 Airplane
• The Aerodynamic Tests of Three Edo Floats for the SB2U-3, 0S2U-2, and XSB2C-2 Seaplanes - NACA Models 106-K, 107-K, and 125-AH
• Aerodynamic Tests of an M-31 Bomb in the 8-Foot High-Speed Tunnel
• Self-Ignition and Combustion of Gases
• High-Speed Tests of a Model Twin-Engine Low-Wing Transport Airplane
• High-Speed Wind-Tunnel Tests of Gun Openings in the Nose of the Fuselage of a 1/4-Scale Model
• Flight Measurements of the Aileron Characteristics of a Grumman F4F-3 Airplane
• Generalized equations for selection charts for heat exchangers in aircraft
• Generalized selection charts for bombers powered by one, two, four, and six 3000-horsepower engines 1: capacity and economy